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Conference 7.286::space

Title:Space Exploration
Notice:Shuttle launch schedules, see Note 6
Moderator:PRAGMA::GRIFFIN
Created:Mon Feb 17 1986
Last Modified:Thu Jun 05 1997
Last Successful Update:Fri Jun 06 1997
Number of topics:974
Total number of notes:18843

225.0. "The Soviet MIR Space Station" by EDEN::KLAES (Mostly harmless.) Thu Oct 23 1986 12:21

VNS TECHNOLOGY WATCH:                           [Mike Taylor, VNS Correspondent]
=====================                           [Nashua, NH, USA               ]

           Soviets Prepare for New Activity on Space Station

      Soviet Union has temporarily halted its manned spaceflight
      activities as the country prepares to begin full-scale
      operations on board its Mir station facility next year when 
      it launches new crews and the first in a series of large
      building block modules. 

      Soviet officials attending the International Astronautical
      Federation's 37th congress said no additional cosmonauts are
      to be sent to Mir in the remaining months of 1986.  the next
      planned manned mission to Mir is planned for early 1987,
      followed by docking of the initial building block, large
      specialized module in the first half of 1987 according to 
      V.V. Ryumin the Soviet manned spaceflight director. 

      First of the specialized modules to be docked will be the
      astrophysics module.  One of the systems on board this module
      will the multinational Complex X-ray Observatory, which uses
      equipment supplied by the Soviet Union, the Netherlands, Great
      Britain, the European Space Agency and West Germany.  the
      facility will view more than 20 targets during its initial
      observation period, including X-ray sources in close binary
      systems, active galaxies, supernova remnants, and galaxy
      clusters. 

      The basic Mir station is 13.1 meters (43 ft) long and has a
      pressurized main cabin, transfer compartment and unpressurized
      service propulsion module. Maximum diameter is 4.2 m (13.8 ft)
      and its mass is 21 metric tons.  The two main engines are
      mounted on the rear and they are covered when not in use.
      Attitude control is provided by 32 reaction control thrusters.
      [How are the main engines used? -mjt] 
      {AW&ST Oct 13,1986}

T.RTitleUserPersonal
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225.1will it be lauch from MIR?PIPA::BIROFri Oct 24 1986 11:32234
------------------------------------------------------------------------------
                   INTERNATIONAL TELECOMMUNICATION UNION
 
                          INTERNATIONAL FREQUENCY
                            REGISTRATION BOARD
 
                                    IFRB
 
_____________________________________________________________________________
					  |
IFRB WEEKLY CIRCULAR/DATE   1740/16.09.86 | SPECIAL SECTION NO. AR11/A/320
__________________________________________|__________________________________
                                          |
SATELLITE NETWORK:     RADIO-M            | RESPONSIBLE ADMNINISTRATION: URS
__________________________________________|__________________________________
 
              INFORMATION RECEIVED BY THE BOARD ON    12.06.86
_____________________________________________________________________________
 
The information contained in this Special Section has been received by the
IFRB pursuant to RR1042 and is published in accordance with RR1044.
 
Any administration which is of the opinion that unacceptable interference 
will be caused to its existing or planned space radio-communications
services will send its comments to the administration concerned, with a
copy to the IFRB, within four months after the date of this publication.
 
            ________________________________________________________
           |                                                        |
           |  EXPIRY DATE FOR THE RECEIPT OF COMMENTS:    16.01.87  |
           |________________________________________________________|
 
 
                   The information reproduced hereunder has
                    been arranged in the form prescribed in 
                      Appendix 4 to the Radio Regulations
 
                        INFORMATION SUPPLIED FOR ADVANCE
                               PUBLICATION FOR THE
                            RADIO-M SATELLITE NETWORK
 
 
General Information
 
	In the U.S.S.R., work is in progress for the development of 
amateur-satellite service systems (ASSS).  In particular, it is planned to
launch one or two amateur satellites, designed for use by radio amateurs
throughout the world and also for educational and scientific experiments.
 
 
Section B  General Characteristics
 
 
Item 1		Identity of the satellite network
 
			RADIO-M
 
 
Item 2		Date of bringing into use
 
			31 December 1986
 
 
Period of validity of frequency assignments to the space station
(Resolution 4, World Administrative Radio Conference, Geneva, 1979)
 
			10 years
 
 
Item 3		Administration or group of administrations submitting the
		advance information
 
		U.S.S.R.
		Ministere des postes et telecommunications
		7, rue Gorki
		MOSKVA
			MINSVIAZ, MOSKVA
 
 
Item 4		Orbital information relating to the space station
 
		Inclination of the orbit:  83 degrees
		Period:			   105 minutes
		Altitude of the apogee:    1 000 km
		Altitude of the perigee:   1 000 km
		Number of satellites:	   1 or 2
 
 
 
Section C	Characteristics of the Satellite Network in the 
		Earth-to-Space Direction
 
 
Item 1		Earth-to-Space service area
 
		The whole Earth, depending on the position of the satellite
		in orbit and the position of the satellite's orbit in
		relation to the Earth.
 
 
Item 2		Class of stations and nature of service
 
		AT, CR
 
 
Item 3		Frequency range
 
		Modes of operation I, II, IV:
 
		21.120 and 21.415 MHz
 
		transponder bandwidth - 40 kHz in one section of the range:
 
		1.  21.260 - 21.300 MHz
		2.  21.210 - 21.250 MHz
		3.  21.160 - 21.200 MHz
 
		Mode of operation III:
 
		145.787 - 146.000 MHz
 
		transponder bandwidth - 40 kHz in one section of the range:
 
		1.  145.960 - 146.000 MHz
		2.  145.910 - 145.950 MHz
		3.  145.860 - 145.900 MHz
 
 
Item 4		Power characteristic of the transmitted wave
 
		These depend upon the design of the station available to the
		amateur.  For good quality relay, an equivalent isotropically
		radiated power (e.i.r.p.) of not more than 100 W will suffice.
 
 
Item 5		Characteristics of the space station receiving antenna
 
		For all modes - a half-wave dipole, gain G = 2 dB, width of
		radiation pattern: 80 degrees.
 
 
Item 6		Noise temperature of the receiving space station
 
		2 000 K
 
 
 
Section D	Characteristics of the satellite Network in the Space-to-Earth
		Direction
 
 
Item 1		Space-to-Earth service area
 
		The whole Earth, depending on the position of the satellite in
		orbit and the position of the satellite's orbit in relation to
		the Earth.
 
 
Item 2		Class of stations and nature of service
 
		EA,CR
 
 
Item 3		Frequency range
 
		Modes of operation I and III:
 
		29.360 - 29.500 MHz
 
		transponder bandwidth - 40 kHz in one section of the range:
 
		1.  29.460 - 29.500 MHz
		2.  29.410 - 29.450 MHz
		3.  29.360 - 29.400 MHz
 
		Mode of operation II:
 
		145.857 - 146.000
 
		transponder bandwidth - 40 kHz in one section of the range:
 
		1.  145.960 - 146.000 MHz
		2.  145.910 - 145.950 MHz
		3.  145.860 - 145.900 MHz
 
		Mode of operation IV:
 
		Simultaneous transmission on the bands 29.360 - 29.500 MHz
		and 145.857 - 146.000 MHz
 
		On each transponder section two beacons operate in the 
		following centre frequencies:
 
		Modes I, III and IV:
 
		1.  29.457 and 29.500 MHz
		2.  29.407 and 29.453 MHz
		3.  29.360 and 29.403 MHz
 
		Modes II and IV:
 
		1.  145.957 and 145.997 MHz
		2.  145.907 and 145.953 MHz
		3.  145.857 and 145.903 MHz
 
 
Item 4		Power characteristics of the transmission
 
		Maximum spectral power density:
 
		29.260 - 29.500 MHz:	-41 dBW/Hz
		145.857 - 146.000 MHz:	-39 dBW/Hz
 
 
Item 5		Characteristics of space station transmitting antenna
 
		For all modes, antenna gain:  1 dB
 
		Radiation pattern:  omnidirectional
 
		Polarization:  linear
 
 
Item 6		Characteristics of receiving earth stations
 
		These depend on the facilities available to amateurs.  It will
		suffice to have a receiving antenna with a gain of 1 to 2 dB
		and a receiving system with an equivalent noise temperature
		of 1 000 K to 1 5 000 K.
------------------------------------------------------------------------------
 noise temperature
		of 1 000 K to 1 5 000 K.
--------------------------------------------
    
225.2GODZLA::HUGHESGary HughesFri Oct 24 1986 11:424
    This weeks issue of Aviation Sneak (Oct 20) has some good photos of Mir
    and Salyut 7, fyi.
    
    gary 
225.3RADIO_M ?PIPA::BIROTue Oct 28 1986 10:3417
    Radio Moscow is playing  up MIR in it news, with reports of
    radio com with the unmaned space spations and agreements with other
    nations on reasearch they will be doing (1988)
    Aviation Leak Also gave some insite to the Communications being
    used they say they are using the 'LURCH' ?sp Satellite
    
    The question I have the orignal plan , according to AMSAT, was that
    HAM SAT M would be launch by MIR, but MIR is in a much lower orbit
    then the proposed plan for RADIO_M.  I can only think of two reasons
    1) it will be launch into a typical Cosmos orbit
    2) it will have a 'kick' motor to put it into a higher orbit
    The previous birds launch via Salyut_7 (ISKAR) were low orbit
    short lived sats, this will be interesing in watching as it would
    be a new feather in the Bear's Hat
    
    jb
    
225.4Radio_M morePIPA::BIROTue Oct 28 1986 10:366
    I think that Radio M will be launch 'piggyback' with a Cosmos
    unit, the reason is the Inclination, MIR is at 51 degrees or so
    and RADIO_M will be at 83 degrees.  I can seem them boasting the
    orbit up with a kick motor but to change the inclination would
    be a tricker job.
    
225.5Will Crew go back to MIR in 86?PIPA::BIROMon Dec 08 1986 18:0315
    I did a quick back of  the match book calculation and if the
    CCCP are indeed to send a crew back to MIR before the end of 
    this year there are only a few window that meet ideal conditions
    (launch in daylight near eveing, and accending orbit -to keep abort
    path in their country, and match with MIR eqx crossing 340 to 343
    degrees or so
    
    If I did my homework right 
    best date  14 th of DEC
    next best  25 th of DEC
    3rd  best  a window around the 20,21st but it is most likly to late
         in the day 
    
    john
    
225.6RE 225.5EDEN::KLAESLooking for nuclear wessels.Mon Dec 08 1986 19:546
    	I cannot guarantee this, but there are several notes in this
    file which state that the Soviets said there will be NO more manned
    flights to the Mir space station in 1986 - but watch out next year!
                                                           
    	Larry
    
225.7Matchbook Calculations?CLOSUS::TAVARESJohn--Stay low, keep movingMon Dec 08 1986 20:403
    RE:.5 Boy I'd like to see that matchbook!  Care to enter a "matchbook"
    describing how you did those calculations?  Something to do while
    we're waiting for SOMEONE to launch...
225.8ENGINE::BUEHLERDirect from the strangoid file.Fri Jan 16 1987 15:116
  I'd like to know the calculation method also - but in layman's terms.
I've never heard or seen what the requisite information is in determining
a launch window and I've always wondered.  It would really be nice if someone
could quickly explain the basics (if possible).

John
225.9CLOSUS::TAVARESJohn--Stay low, keep movingFri Jan 16 1987 15:394
Yeah!  After re-reading my note asking for the matchbook calculations,
I realize that I may have sounded sarcastic.  Actually, I am in awe of
anything mathematical, and am very interested in such a procedure.  My
HP11 stands ready...
225.10FROM PYRITE::ASTRONOMY - ORBITAL CALCULATIONSEDEN::KLAESAlchemists get the lead out.Fri Jan 16 1987 16:0688
           <<< LDP::SYS$SYSDEVICE:[NOTES$LIBRARY]ASTRONOMY.NOTE;1 >>>
                         -< Astronomical Discussions >-
================================================================================
Note 241.2                      Japanese Ball?                            2 of 3
VIDEO::COHAN "Mort Cohan, PKO3-1/10C"                79 lines  14-JAN-1987 17:16
                           -< MIR possible in Mass. >-
--------------------------------------------------------------------------------

1
     AMSAT Elliptical Orbit Calculator
     V. 41, VAX FORTRAN adaptation by KA1IU, of W3IWI BASIC Program
     Copyright 1983, 1984 by AMSAT, W3IWI, KA1IU


     Reference Epoch:  1987 +    1.853952960

     Starting Epoch:   1987 +    8.937500000
                       MON/DAY/YR= 1/ 8/87 at 22:30 UTC

     Element Set  3: MIR (86-17A) (OBJ 16609 Set: 430) 

     Fundamental Keplerian Elements:

                              At Reference             At Start

     Mean Anomaly deg         86.045200000             61.967673888
     Inclination deg          51.614500000
     Eccentricity              0.002049700
     Mean Motion rev/day      15.800607800             15.803083783
     Arg. Perigee deg        273.823000000            301.237425544
     R.A.A.N. deg            290.870300000            254.178548929

     Other Parameters:

     Orbit Number           4986                     5098
     S.M.A. km              6708.363                 6707.663
     Apogee Height km        343.953
     Perigee Height km       316.453
     Anom. Period min         91.136
     Decay Rate rev/day^2      1.748E-04
     Doppler Freq mhz        143.625


     Argument of perigee will rotate 360 degrees
     in about     0 years,  93 days.

     Earth angle subtended:      Apogee   Perigee
                                   36.8      35.4 deg

     For observer at   42.2 deg lat,    71.3 deg long,
     visibility circle at average of apogee and perigee height is:

       Northern limit:    60.2 deg latitude
       Center:            40.9
       Southern limit:    24.1

     (Values>90 are on far side of pole. Negative=South Lat.)
     (Center is for circle on stereographic map projection.)


     Exact time of apogee indicated by A after UTC in output.
1
     E Mass  Lat=   42.153 Long=   71.283  Ht=  60.m  Window Limit=
     0.0 deg      Element Set  3: MIR (86-17A) (OBJ 16609 Set: 430) 

     Doppler shift calculated for    143.625 mhz

     Current     Arg Perigee        R.A.A.N.          Period          S.M.A.
                    301.3020        254.0922         91.1214        6707.661

     Eqx Time = ****:**             Eqx Long = ******

      U.T.C.    AZ   EL  DOPPLER  RANGE   HEIGHT   LAT   LONG  PHASE
     HHMM:SS   deg  deg     hz      km      km    N+S-   W+E-  <256>
      1/ 8/87 THU               -----DAY #   8----ORBIT #   5098----
     2254:00   307  0.6    3310    2089     342   50.9   94.3   111
     2255:00   310  4.9    3280    1677     342   50.0   88.5   114
     2256:00   314   11    3200    1272     343   48.9   83.0   117
     2257:00   322   20    2979     889     343   47.4   77.8   120
     2258:00   344   36    2247     573     343   45.8   72.8   123
     2259:00    49   45    -226     487     343   43.9   68.2   126
     2259:53A   87   29   -2891     679     343   42.0   64.4A  128
     2300:00    90   27   -2614     718     343   41.8   63.9   128
     2301:00   102   15   -3200    1079     343   39.5   59.9   131
     2302:00   108  7.4   -3317    1476     343   37.1   56.2   134
     2303:00   111  2.5   -3321    1886     343   34.6   52.7   137
     2304:00   113 -1.4   -3325    2300     343   31.9   49.5   140

225.11progess-27 docks with MIRIMNAUT::BIROMon Jan 19 1987 12:0034
    Over the weekend Radio Moscow announce the following
    Progress-27 (I added 27 as it is the next one in the series)
    cargo spacecraft auto dockedwith the orbiting space sation MIR.
    It brough fuel and supplies for next man mission.  They went on
    to say that an internation crew is being traied at STAR_TOWN (I
    am not sure if this is an error or a new training center as it was
    called STAR_CITY before) in pre for permanent maning of MIR.
    --------------
    
    Now with both MIR/P-27 it should be a super visual site but present
    passes are mostly in the daytime except for a few early AM ones
    on the East Coast of the US
    The next window for man launch is late feb or early march
    The caluclation is quite simple , the equation was worked out
    by the Boy's school in Eng  ( I think ?sp Kittering Group )
    
    launch time = (eqx time in min) + 10.8  + 4 * (347.5 - eqx long
                            of the space station)
    
    However this was for a 24 hour trip from ground to the space station
    and now with incress load/supplies to say fule they are doing it
    in 48 hours so the eq is not right but close
    
    
    things to look for in a man launch is a perfered time abt 1200 utc
    an accending orbit and a crossing around 340-344 deg w of the equator
    from the space station
    
    the reson for all the above is in case of an abort the unit will
    come down in CCCP territory and in the daylate but late eve
    
    jb
    
    
225.12unman calculationsIMNAUT::BIROMon Jan 19 1987 16:3917
    for unmaned launch the eq crossing should be about
    334 to 339
    
    best fit for 1/16/87 would be
    orbit # 5213 
    eqx time 05:01:00.495
    eqx long 333.9 degrees W
    
    thus if the equation is still good for 48 trips
    t0 = (5*60 +1) + 10.8 + 4*(347.5-333.9)
    t0 = 6 hours 6 min and 12 sec
    
    in will be interesting to see if they publish the exact launch time
    and see how close this comes
    
    jb
    
225.13JANUS::BARKERTue Jan 20 1987 09:2315
re: .11

The group in England is the Kettering Group.  The group was started about 
1960 by the physics teacher at the school who ran the group as a lunchtime 
activity for many years.  I think the teacher retired a few years ago.

The group observes Soviet spacecraft through the means of monitoring radio
communications.  They determine orbits by measuring doppler shift. Among
their acheivements are the announcement of the use of and location of the
Plesetsk launch site (through back calculation from orbit data) when the
CIA and NSA thought only they knew and considered the information highly
classified, and the decoding of telemetry signals from various series of
scientific satellites and manned spacecraft. 

Jeremy Barker - Reading, England
225.14and the launch time was ?IMNAUT::BIROWed Jan 28 1987 11:1516
    ok either the formular is no good for 24 hour trips or Aviation
    Week got pm and am mixed up
    
    this week AW had the P-27 launch at 09:06 PM Moscow time
    if I am right there is 3 hours diff between MOSCOW time and
    UTC so that would make it 06:06 UTC (PM)
    the numbers match exactly but it is pm not am so that put the
    launch at 18:06 UTC,
    
    will look over the launch opportunity at 1800 utc but it does
    not look right, I think AW got PM and AM mixed
    
    any ideas?
    
    jb
    
225.151st Anniversary of MIRIMNAUT::BIROThu Jan 29 1987 16:5217
    a very interesting launch, it turns out that there are two launch
    window, one of the ascending orbit (ground track of MIR) and the
    one on the desending orbit.  P27 was launch on the descending ground
    track of MIR, both solutions are valid but the Kettering Group formular
    was base on the fact that one of the rules would be ascending launchs
    only.  
    
    Now to make another educated guess on the next maning of MIR, I
    think that unless they change the orbit of MIR (as AW suggest they
    will do ) and with the fact that there is a MAN window opening near
    the end of FEB that the Russian will try for the 1st annerversary
    of MIR for the new crew  Yuri Romanenko (42) and Alexander Laveikin
    
    The 1st Anniversary will be   the  20 th of FEB 87
    
    jb
    
225.16Was the tower stored in S7IMNAUT::BIROWed Feb 04 1987 15:2511
    On May 28, 1986, the cosmonauts aboard Salyut 7 unfolded a 15 meter
    long tower.  The tower was collapsed back into the canister. The
    tower deployment was then repeated during a second spacewalk on
    the 31st of May. This time it was raised to 12 meters while instruments
    measured its movement under stress. The tower again was retraceted
    but a few joints were welded togeter.  My question to anyone is
    I am not sure but I think the tower was then stored inside S7 as
    they closed out the old Salyut 7.
    
    jb
    
225.17TM2 to launch thur/fri15797::BIROWed Feb 04 1987 22:4754
Associated Press Wed  4-FEB-1987 14:50             Soviet-Space

 4-FEB-8714:50

Soviet Space Launch Set for Friday
   MOSCOW (AP) - Two cosmonauts will be launched Friday on the
first Soviet manned space flight since last summer, Tass said
Wednesday.
   The Soyuz TM-2 spacecraft carrying cosmonauts Yuri Romanenko and
Alexander Laveikin will be launched from the Baikonur space center
in Central Asia at 12:38 a.m. Moscow time (4:38 a.m. EST) Friday,
the official news agency reported.
   The cosmonauts are expected to dock with the Mir orbiting space
station, which has been unmanned since July, when the last Soviet
manned space mission was completed.
   Soviet officials have not said how long the TM-2 mission will
last, but there are signs that the two cosmonauts may stay in space
for at least six months. Earlier Soviet press reports said that
there would be one manned craft launched in early 1987 and a second
one in July, with cosmonauts from both missions spending time
together at the Mir station.

******  OK HOW TO YOU PREDICT THE LAUNCH TIME
Element Set  3: MIR (86-17A) (OBJ 16609 Set: 462)
     Element Set  3: MIR (86-17A) (OBJ 16609 Set: 462)                           

        Date    Orbit       Eqx Time    Eqx Long   Nodal Period   Del Eqx Long

      2/ 5/87    5536    1605:31.841       265.9       91.37640       23.23312
      2/ 5/87    5537    1736:54.420       289.1       91.37632       23.23294
      2/ 5/87    5538    1908:16.999       312.3       91.37632       23.23227
      2/ 5/87    5539    2039:39.568       335.6       91.37614       23.23323

>     2/ 5/87    TM2     2138:00.000       PROPOSED SOYUZ TM2 LAUNCH
MIR   2/ 5/87    MIR     2138:00    IS AT -36.6 LAT AND 134.3 LONG 

      2/ 5/87    5540    2211:02.136       358.8       91.37613       23.23240
      2/ 5/87    5541    2342:24.698        22.0       91.37604       23.23267
      2/ 6/87    5542    0113:47.252        45.3       91.37590       23.23311
      2/ 6/87    5543    0245:09.808        68.5       91.37593       23.23208
      2/ 6/87    5544    0416:32.353        91.7       91.37576       23.23299


FORM THE EQUATION

To = (eqx time in min) + 10.8 + 4 * (347.5 -eqx long)
To = (1239.66) + 10.8 + 4 * (11.9)
To = 21 Hours 38 min and 4 sec

73's jb

    ok so a night launch, this mean the TM has to stay in orbit for
    3 revolutions before it can ditch in homeland
    
225.18MIR VHF radios are on15797::BIROMon Feb 09 1987 11:1313
    Docking happen at 23:28 utc on Sat, about 4 hours later I receive
    VHF communicaiton from MIR to the Soviet Ships near SAble Island
    
    Before docking the crew took a complet circle around MIR then docked
    RM  (radio Moscow) said that the Computers onboard both MIR and
    Soyuz TM2 were use in a new system to min the amount of fuel required
    for docking, they gave it a name and will try to get the correcting
    spelling of it..  I heard no communicaitons on Sunday but they seem
    to be back on normal work schedule this AM as I pick up two pass
    with VHF communications.  The previous MIR crew seem to work from
    about 1000 utc to 1800 utc . 
    jb
    
225.19MIR in ViennaMTWAIN::KLAESAll the Universe, or nothing!Wed Sep 18 1991 20:1846
Article        35753
From: roberts@CMR.NCSL.NIST.GOV (John Roberts)
Newsgroups: sci.space
Subject: Mir in Vienna?
Date: 18 Sep 91 18:07:04 GMT
Sender: daemon@ucbvax.BERKELEY.EDU
Organization: National Institute of Standards and Technology
 
        A friend at work went to Vienna a few weeks ago, and came back
    with a photograph he took of a Mir, sitting out in the open, apparently 
    along a road or in a park.  It has a wall around it, but apparently is on 
    a platform, so it can be seen above the wall.  There's a walkway the length 
    of the station, with a gap in the wall and steps to reach the walkway.  
    The station structure is linear, and appears to be two big cylinders with 
    interconnections of smaller cylinders, and a small spherical component at 
    one end with lots of small rocket nozzles.  In volume it appears to be 
    about like 3.5-4 VW Microbuses connected end to end.  It might be possible 
    to "stand" perpendicular to the axis of the craft in one of the large 
    cylinders, but it's hard to tell. 
 
        On the walls around the Mir are posters with (approximately) the
    following: 
 
    UNITERRA
    WORLD TECH
    VIENNA
    KOMMUNALWIRTSCHAFT 91
    23-27 Okt. 91 Messegelande
 
    DIE CHRUNITSCHEW-WERKE [unreadable]
    PRASENTIEREN DIE
    WELTRAUMSTATION M/P    [not sure that's a '/']
            KOMM ZU MIR
 
    and next to the walkway where it's between the two large cylinders:
 
    AUFGANG
    ZUR  [?]
    ORBITALSTATION
    MIR
 
    Can anyone translate/explain what's going on?
 
    John Roberts
    roberts@cmr.ncsl.nist.gov

225.20RE 225.19MTWAIN::KLAESAll the Universe, or nothing!Fri Sep 20 1991 14:49105
Article        35808
From: davew@sputnik.mit.edu (dave warkentin)
Newsgroups: sci.space
Subject: Re: Mir in Vienna?
Date: 19 Sep 91 22:32:29 GMT
Sender: news@athena.mit.edu (News system)
Organization: M.I.T.
 
In article <9109181807.AA00417@cmr.ncsl.nist.gov>,
roberts@CMR.NCSL.NIST.GOV (John Roberts) writes:

 > [description of what is presumably a mock-up of a Mir deleted]
 > 
 > On the walls around the Mir are posters with (approximately) the following:
 > 
 > UNITERRA
 > WORLD TECH
 > VIENNA
 > KOMMUNALWIRTSCHAFT 91
 > 23-27 Okt. 91 Messegelande

It looks like the Kommunalwirtschaft '91 trade show/convention will 
be held on the convention grounds (Messegelaende) near Vienna this
October 23-27.  I believe Kommunalwirtschaft means something like local
or municipal economy/ business.  Uniterra and World Tech may be
participants or perhaps co-sponsors.  I'm not sure why Vienna is
spelled that way - in German it's Wien. 

 > DIE CHRUNITSCHEW-WERKE [unreadable]
 > PRASENTIEREN DIE
 > WELTRAUMSTATION M/P    [not sure that's a '/']
 >         KOMM ZU MIR

The Krunichev (hard to tell the anglicized spelling from the German
version) factories present the space station Mir (they used the
cyrillic which looks like MIP).  Come to me.  (A pun - "me" in German
is "mir".) 
 
 > and next to the walkway where it's between the two large cylinders:
 > 
 > AUFGANG
 > ZUR  [?]
 > ORBITALSTATION
 > MIR

Entrance (actually "the way up" more or less) to the orbital station
Mir. ("zur" is correct - it's a contraction of "zu der" or "to the".)
 
 > Can anyone translate/explain what's going on?
 > 
 > John Roberts
 > roberts@cmr.ncsl.nist.gov

Hope this helps.
--
Dave Warkentin
davew@sputnik.mit.edu

Article        35813
From: 3001crad@ucsbuxa.ucsb.edu (Charles Frank Radley)
Newsgroups: sci.space
Subject: Re: Mir in Vienna?
Date: 20 Sep 91 00:21:26 GMT
Sender: root@ucsbcsl.ucsb.edu
 
In article <9109181807.AA00417@cmr.ncsl.nist.gov>
roberts@CMR.NCSL.NIST.GOV (John Roberts) writes: 

>UNITERRA
>WORLD TECH
>VIENNA
>KOMMUNALWIRTSCHAFT 91
>23-27 Okt. 91 Messegelande
 
This is announcing an exhibition called "Uniterra" to be held at the
"Messegelande" = Exhibtion palace; date 23 - 27 October 91. Or else
Uniterra is the sponsoring organization. "Kommunalwirtschaft"
transliterate as "Communal Commerce" 
 
>DIE CHRUNITSCHEW-WERKE [unreadable]
>PRASENTIEREN DIE
>WELTRAUMSTATION M/P    [not sure that's a '/']
>        KOMM ZU MIR
 
"the Chrunitschew-Factory ----- presents the Space Station M/P Come to Mir" 
 
>and next to the walkway where it's between the two large cylinders:
 
>AUFGANG
>ZUR  [?]
>ORBITALSTATION
>MIR
 
Did it really say "Aufgang" ?  Ausgang = exit.
Aufgang = excursion.
  It is either " Exit (or) Excursion to the Mir orbital station."
 
>Can anyone translate/explain what's going on?
 
My transliteration attempt was from memory, with no dictionary.
I hope it is fairly accurate.
 
>John Roberts
>roberts@cmr.ncsl.nist.gov

225.21MIR History, February 1986 to July 1989VERGA::KLAESSlaves to the Metal HordesFri Jul 17 1992 15:20198
Article: 46116
From: tfreer@metz.une.edu.au (TIMOTHY FREER)
Newsgroups: sci.space
Subject: Mir diary pt.1
Date: 17 Jul 92 05:42:21 GMT
Sender: usenet@grivel.une.edu.au
 
MIR DIARY Pt.1 (Feb 1986 to July 1989)
-------------------------------
    This is the first in a series of 'Salyut' diaries that I will be
presenting. The purpose of these is that they will provide readers
with an accurate reference, which lists all major events surrounding
Soviet/CIS space station activities since 1977. 

    This first diary lists major events involving the Mir space
station during it's first three years of manned operations. This
period begins with the launch of the core module in February 1986, and
ends with the four month gap in manned activities during mid 1989.
Listed are all launches to Mir, all dockings, port transfers, space
walks, undockings, and re-enries, that occured during this period. All
dates are in GMT , and are reasonably accurate. If you have any
corrections, please post them to me with your sources. 
 
 ---------------------------------------------------------------------------
 Mir diary pt.1 (Feb86 to Jul89).
----------------------------------------------------------------------------
 1986
----------------------------------------------------------------------------
19 FEB    Mir launched by Proton rocket into 172 x 301km orbit at 51.6 
          degrees inclination.
06 MAR    Mir established in its 332 x 342km operational orbit.
13 MAR    Soyuz T-15 launched with Leonid Kizim and Vladimir Solovyev aboard.
15 MAR    Soyuz T-15 docks with the extreme forward port.
19 MAR    Progress 25 launched.
21 MAR    Progress 25 docks with the rear port.
17 APR    Mir's orbit adjusted to match Salyut-7's - the two laboratories
          are now flying in formation at 4000km separation to avoid radio-
          interference.
20 APR    Progress 25 undocks and is directed into the atmosphere to burn up.
23 APR    Progress 26 launched.
25 APR    Progress 26 unable to dock because of problems with Mir's radio-
          communications system.
26 APR    Progress 26 docks with the rear port.
04 MAY    Mir's orbit is lowered, causing it to catch up with Salyut-7.
05 MAY    Soyuz T-15 undocks, carrying Kizim and Solovyev across to Salyut-7.
21 MAY    Soyuz TM, an updated design of the Soyuz T craft, launched on an
          unmanned test mission.
23 MAY    Soyuz TM docks with the extreme foward port.
29 MAY    Soyuz TM undocks.
30 MAY    Soyuz TM re-enters unmanned.
22 JUN    Progress 26 undocks.
23 JUN    Progress 26 directed into the atmospere to burn up.
25 JUN    Soyuz T-15 leaves Salyut-7 with Kizim and Solovyev aboard.
26 JUN    Soyuz T-15 docks for a second time with the extreme forward port.
16 JUL    Soyuz T-15 undocks and re-enters with Kizim and Solovyev aboard.
----------------------------------------------------------------------------
 1987.
----------------------------------------------------------------------------
16 JAN    Progress 27 launched.
18 JAN    Progress 27 docks with the rear port.
05 FEB    Soyuz TM-2 launched with Yuri Romanenko and Alexsandr Laveikin
 
          aboard.
07 FEB    Soyuz TM-2 docks with the extreme forward port.
23 FEB    Progress 27 undocks.
25 FEB    Progress 27 directed into the atmosphere to burn up.
03 MAR    Progress 28 launched.
05 MAR    Progress 28 docks with the rear port.
26 MAR    Progress 28 undocks.
28 MAR    Progress 28 directed into the atmosphere to burn up.
31 MAR    Kvant-1 module, carrying the Rontgen astrophysical observatory,
          launched by Proton rocket.
06 APR    Kvant-1 arrives, but a problem on its final approach to Mir causes
          the docking to be postponed.
09 APR    Kvant-1 links-up with the rear port, but an obstruction in its
          docking unit prevents the two craft from being sealed together.
11 APR    Romanenko and Laveikin make a 3 hour 40 minute spacewalk to examine
          the docking units of Mir and Kvant-1 - Laveikin removes 'a twisted
          piece of cloth', and ground control completes the docking by remote
          control while the cosmonauts look on.
12 APR    Kvant-1's 'space tug' departs, leaving a new docking unit open at
          the rear of the complex.
21 APR    Progress 29 launched.
23 APR    Progress 29 docks with Kvant-1's rear port, creating the worlds
          first four-spacecraft link-up.
11 MAY    Progress 29 undocks and is directed into the atmospere to burn-up.
19 MAY    Progress 30 launched.
21 MAY    Progress 30 docks with Kvant-1's rear port.
12 JUN    Romanenko and Laveikin make a 1 hour, 53 minute spacewalk to
          commence the assembly of a third panel of solar cells on the 
          outside of Mir.
16 JUN    Romanenko and Laveikin make a 3 hour, 15 minute spacewalk to
          complete assembly work on the solar panel.
?? JUL    Prorgess 30 undocks and is directed into the atmosphere to burn-up.
22 JUL    Soyuz TM-3 launched with Aleksandr Viktorenko, Alexsandr
          Alexsanderov and Muhammand Faris (Syria) aboard.
24 JUL    Soyuz TM-3 docks with Kvant-1's rear port.
29 JUL    Soyuz TM-2 undocks carring Viktorenko, Faris and Laveikin,
          returning because of 'an irregularity in his heart rhythm'.
30 JUL    Soyuz TM-2 re-enters.
30 JUL    Soyuz TM-3 is transfered from Kvant-1's rear port to Mir's
          extreme forward port by Romanenko and Alexanderov.
03 AUG    Progress 31 launched.
05 AUG    Progress 31 docks with Kvant-1's rear port.
21 SEP    Progress 31 undocks and is directed into the atmosphere to burn-up.
23 SEP    Progress 32 launched.
26 SEP    Progress 32 docks with Kvant-1's rear port.
10 NOV    Progress 32 undocks from Kvant, edocking 98 minutes later in a test
          of new fuel saving software for Mir.
17 NOV    Progress 32 undocks and is directed into the atmosphere to burn-up.
20 NOV    Progress 33 launched.
23 NOV    Progress 33 docks with Kvant-1's rear port.
19 DEC    Progress 33 undocks and is directed into the atmosphere to burn-up.
21 DEC    Soyuz TM-4 launched with Vladimir Titov, Musakhi Manarov and
          Alexsandr Levchenko aboard.
23 DEC    Soyuz TM-4 docks with Kvant-1's rear port.
29 DEC    Soyuz TM-3 undocks and re-enters carring Romanenko, Alexsanderov
          and Levchenko. Romanenko sets new endurance record.  
30 DEC    Soyuz TM-4 is transfered to Mir's extreme forward port by Titov
          and Manarov.
----------------------------------------------------------------------------
 1988.
----------------------------------------------------------------------------
20 JAN    Progress 34 launched.
23 JAN    Progress 34 docks with Kvant-1's rear port.
26 FEB    Titov and Manarov make a 4 hour, 25 minute spacewalk to install an
          experimental solar cell on the third solar panel outside Mir.
04 MAR    Progress 34 undocks and is directed into the atmosphere to burn-up.
23 MAR    Progress 35 launched.
25 MAR    Progress 35 docks with Kvant-1's rear port.
05 MAY    Progress 35 undocks and is directed into the atmosphere to burn-up.
13 MAY    Progress 36 launched.
15 MAY    Progress 36 docks with Kvant-1's rear port.
05 JUN    Progress 36 undocks and is directed into the atmosphere to burn-up.
07 JUN    Soyuz TM-5 launched with Anatoly Solovyov, Viktor Savinykh and
          Alexsandr Alexsanderov (Bulgaria) aboard.
09 JUN    Soyuz TM-5 docks with Kvant-1's rear port.
17 JUN    Soyuz TM-4 undocks and re-enters carring Solovyov, Savinykh and
          Alexsanderov.
18 JUN    Soyuz TM-5 is transfered to Mir's extreme forward port by Titov
          and Manarov.
30 JUN    Titov and Manarov make a 5 hour, 10 minute spacewalk to commence
          repairs on the Kvant-1 module.
18 JUL    Progress 37 launched.
20 JUL    Progress 37 docks with Kvant-1's rear port.
12 AUG    Progress 37 undocks and is directed into the atmosphere to burn-up.
29 AUG    Soyuz TM-6 launched with Valery Lyakhov, Valery Poliakov and Abdol
          Muhamand (Afghanistan) aboard.
31 AUG    Soyuz TM-6 docks with Kvant-1's rear port.
05 SEP    Soyuz TM-5 undocks with Lyakhov and Muhamand aboard.
06 SEP    Soyuz TM-5 re-entry delayed 24 hours by retro-rocket malfunction.
07 SEP    Soyuz TM-5 lands.
08 SEP    Soyuz TM-6 is transfered to Mir's extreme forward port by Titov,
          Manarov and Poliakov.
09 SEP    Progress 38 launched.
12 SEP    Progress 38 docks with Kvant-1's rear port.
20 OCT    Titov and Manarov make a 4 hour, 12 minute spacewalk to complete
          repairs on the Kvant-1 module.
23 NOV    Progress 38 undocks and is directed into the atmosphere to burn-up.
26 NOV    Soyuz TM-7 launched with Alexsandr Volkov, Sergei Krikalyov and
          Jean-Loup Chretien (France) aboard.
28 NOV    Soyuz TM-7 docks with Kvant-1's rear port.
09 DEC    Volkov and Chretien make 5 hour, 7 minute spacewalk to install
          French instruments. First spacewalk by a French 'spationaut'.
21 DEC    Soyuz TM-6 undocks and re-enters with Titov, Manarov and Chretien
          aboard. Titov and Manarov establish a new endurance record of 
          365 days in orbit.
21 DEC    Soyuz TM-7 transfered to Mir's extreme forward port by Volkov,
          Krikalyov and Poliakov.
25 DEC    Progress 39 launched.
27 DEC    Progress 39 docks with Kvant-1's rear port.
----------------------------------------------------------------------------
 1989.
----------------------------------------------------------------------------
07 FEB    Progress 39 undocks and is directed into the atmosphere to burn-up.
10 FEB    Progress 40 launched.
12 FEB    Progress 40 docks with Kvant-1's rear port.
03 MAR    Progress 40 undocks and is directed into the atmosphere to burn-up.
16 MAR    Progress 41 launched.
18 MAR    Progress 41 docks with Kvant-1's rear port.
25 APR    Progress 41 undocks and is directed into the atmosphere to burn-up.
27 APR    Soyuz TM-7 undocks and re-enters with Volkov, Krikalyov and
          Poliakov aboard. Mir left vacant.
----------------------------------------------------------------------------
----------------------------------------------------------------------------
end.    My next diary will be Mir pt.2, which will list major events
     involving Mir from Aug89 to Jul92. In the near future I will also be
     posting diaries for Salyut-7 and Salyut-6 operations.
 
                                      Bye for now Tim Freer.

    "[The space program] can help counter the head-on collision with the 
  environmental chaos we now face; spearhead technological, competitive, 
  and political leadership; stimulate young minds to excellence; and forge 
  cultural bonds between nations for the benefit of all humanity." 

                             - Leonard David 

225.22MIR History, August 1989 to July 1992VERGA::KLAESSlaves to the Metal HordesFri Jul 17 1992 16:28199
Article: 46128
From: tfreer@metz.une.edu.au (TIMOTHY FREER)
Newsgroups: sci.space
Subject: Mir diary pt.2
Date: 17 Jul 92 14:02:11 GMT
Sender: usenet@grivel.une.edu.au
 
MIR DIARY Pt.2 (Aug 1989 to July 1992)
-------------------------------
 
    This diary continues on from my first posting, listing major
events during manned operations with the Mir space station between
August 1989 and July 1992. Once again the listing includes all
launches to Mir, all dockings, port transfers, spacewalks, undockings
and re-entries, that occured during this period. All dates are in GMT,
and are reasonably accurate. 

    I trust that you will find this diary a usefull reference for
major Mir space station activities. If you have any corrections,
please post them to me. 
 
-----------------------------------------------------------------------------
 Mir diary pt.2 (Aug89 to Jul92).
-----------------------------------------------------------------------------
 1989.
-----------------------------------------------------------------------------
23 AUG    Progress M launched.
25 AUG    Progress M docks with Mir's extreme forward port.
05 SEP    Soyuz TM-8 launched with Alexsandr Viktorenko and Alexsandr
          Serebrov aboard.
07 SEP    Soyuz TM-8 docks with Kvant-1's rear port.             
26 NOV    Kvant 2 launched by Proton rocket.
01 DEC    Progress M undocks and is directed into the atmosphere to burn-up.
02 DEC    Kvant-2 aborts attempted docking with Mir.
06 DEC    Kvant-2 docks with Mir's extreme forward port.
08 DEC    Kvant-2's 'Ljappa' manipulator is used to transfer Kvant-2 to the
          upper port on Mir's forward docking unit.
12 DEC    Soyuz TM-8 transfered to Mir's extreme forward port by Viktorenko,
          and Serebrov.
20 DEC    Progress M-2 launched.
22 DEC    Progress M-2 docks with Kvant-1's rear port.
----------------------------------------------------------------------------
 1990.
----------------------------------------------------------------------------
09 JAN    Viktorenko and Serebrov make a 2 hour, 56 minute spacewalk to
          install sensors outside the Mir core module.
11 JAN    Viktorenko and Serebrov make a 2 hour, 54 minute spacewalk to
          retrieve French instruments and to prepare the extreme forward
          docking port for the arrival of Kristall.
26 JAN    Viktorenko and Serebrov install camera equipment outside Kvant-2
          in a 3 hour, 2 minute spacewalk.
01 FEB    Viktorenko and Serebrov make a 4 hour, 59 minute spacewalk.
          Serebrov makes first test of 'Space Motorcycle'.
05 FEB    Viktorenko and Serebrov make a 3 hour, 45 minute spacewalk.
          Viktorenko tests 'Space Motorcycle'.
09 FEB    Progress M-2 undocks and is directed into the atmosphere to burn-up.
11 FEB    Soyuz TM-9 launched with Anatoli Solovyov and Alexsandr Balandin
          aboard.
13 FEB    Soyuz TM-9 docks with Kvant-1's rear port.
18 FEB    Soyuz TM-8 undocks and re-enters with Viktorenko and Serebrov       
          aboard.
21 FEB    Soyuz TM-9 transfered to Mir's extreme forward port by Solovyov 
          and Balandin.
28 FEB    Progress M-3 launched.
03 MAR    Progress M-3 docks with Kvant-1's rear port.
27 APR    Progress M-3 undocks and is directed into the atmosphere to burn-up.
05 MAY    Progress 42 launched (last of original design).
07 MAY    Progress 42 docks with Kvant-1's rear port.
27 MAY    Progress 42 undocks and is directed into the atmosphere to burn-up.
28 MAY    Soyuz TM-9 transfered to Kvant-1's rear port by Solovyov and 
          Balandin.
31 MAY    Kristall launched by Proton rocket.
06 JUN    Kristall's docking with Mir is postponed because of problems with
          Kristall's orientation motors.
10 JUN    Kristall docks with Mir's extreme forward port.
11 JUN    Kristall's 'Ljappa' manipulator is used to transfer the module to
          the lower port on Mir's forward docking unit opposite Kvant-2.
03 JUL    Soyuz TM-9 transfered to Mir's extreme forward port by Solovyov,
          and Balandin.
17 JUL    Solovyov and Balandin make a 7 hour spacewalk to repair damaged
          insulation blankets on Soyuz TM-9. Problems experienced in
          re-entering Kvant-2.
26 JUL    Solovyov and Balandin make a 3 hour, 31 minute spacewalk to close
          jammed hatch on Kvant-2, and complete repairs to Soyuz TM-9.
01 AUG    Soyuz TM-10 launched with Gennadi Manakov and Gennadi Strekalov
          aboard.
03 AUG    Soyuz TM-10 docks with Kvant-1's rear port.
09 AUG    Soyuz TM-9 undocks and re-enters with Solovyov and Balandin     
          aboard.
15 AUG    Progress M-4 launched.
17 AUG    Progress M-4 docks with Mir's extreme forward port.
??????    Progress M-4 undocks and is directed into the atmosphere to     
          burn-up.
27 SEP    Progress M-5 launched.
29 SEP    Progress M-5 docks with Mir's extreme forward facing port.
??????    Manakov and Strekalov make unsuccesfull spacewalk to repair
          Kvant-2's damaged hatch.
28 NOV    Progress M-5 undocks and is directed into the atmosphere to
          burn-up. Recoverable capsule re-enters.
02 DEC    Soyuz TM-11 launched with Viktor Afanaseyev, Musakhi Manarov,
          and Toyohiro Akiyama (Japan) aboard.
04 DEC    Soyuz TM-11 docks with Mir's extreme forward facing port.
10 DEC    Soyuz TM-10 undocks and re-enters with Manakov, Strekalov, and
          Akiyama aboard.
---------------------------------------------------------------------------
 1991.
---------------------------------------------------------------------------
07 JAN    Afanaseyev and Manarov repair Kvant-2's damaged hatch in 
          a 5 hour, 18 minute spacewalk.
14 JAN    Progress M-6 launched.
16 JAN    Progress M-6 docks with Kvant-1's rear port.
23 JAN    Afanaseyev and Manarov make spacewalk to install an extendable
          boom on Kvant-2's exterior.
26 JAN    Afanaseyev and Manarov complete installment of equipment in a
          6 hour, 20 minute spacewalk.
15 MAR    Progress M-6 undocks and is directed into the atmosphere to burn-up.
19 MAR    Progress M-7 launched.
21 MAR    Progress M-7 unsuccesfull in docking attempt because of computer
          error.
23 MAR    Progress M-7 passes within five metres of Mir during second docking
          failure caused by malfunctioning Kurs rendevous system.
26 MAR    Soyuz TM-11 transfered Afanaseyev and Manarov to Kvant-1's rear
          port to test Kurs system.
28 MAR    Progress M-7 docks with Mir's extreme forward port.
25 APR    Afanaseyev and Manarov make a 3 hour, 34 minute spacewalk to 
          collect samples and photograph the Kurs antenna.
07 MAY    Progress M-7 undocks and is directed into the atmosphere to burn-up.
18 MAY    Soyuz TM-12 launched with Anatoli Artsebarski, Sergei Krikalyov,
          Helen Sharman (United Kingdom) aboard.
20 MAY    Soyuz TM-12 docks with Mir's extreme forward facing port.
26 MAY    Soyuz TM-11 undocks and re-enters with Afanaseyev, Manarov and
          Sharman aboard.
28 MAY    Soyuz TM-12 transfered to Kvant's rear port by Artsebarski and
          Krikalyov.
30 MAY    Progress M-8 launched.
01 JUN    Progress M-8 docks with Mir's extreme forward port.
25 JUN    Artsebarski and Krikalyov make a 4 hour, 58 minute spacewalk to
          repair Kurs antenna.
29 JUN    Artsebarski and Krikalyov make a 4 hour, 58 minute spacewalk to
          deploy a U.S cosmic ray detector.
15 JUL    Artsebarski and Krikalyov make a 5 hour, 50 minute spacewalk to
          begin building a space girder.
19 JUL    Artsebarski and Krikalyov make fourth spacewalk.
23 JUL    Artsebarski and Krikalyov make fifth spacewalk.
27 JUL    Artsebarski and Krikalyov make sixth spacewalk.
16 AUG    Progress M-8 undocks and is directed into the atmosphere to
          burn-up. Experiment to deploy baloon from freighter failed.
20 AUG    Progress M-9 launched.
23 AUG    Progress M-9 docks with extreme forward port.
30 SEP    Progress M-9 undocks and is directed into the atmosphere to     
          burn-up. Recoverable capsule re-enters.
02 OCT    Soyuz TM-13 launched with Alexsandr Volkov, Tokhtar Aubakirov
          (Khazakstan), and Franz Viehbock (Austria) aboard.
04 OCT    Soyuz TM-13 docks with Mir's extreme forward facing port.
10 OCT    Soyuz TM-12 undocks and re-enters with Artsebarski, Aubakirov
          and Viehbock aboard.
15 OCT    Soyuz TM-13 transfered to Kvant-1's rear port by Volkov and
          Krikalyov.
17 OCT    Progress M-10 launched.
19 OCT    Progress M-10 aborts docking sequence.
21 OCT    Progress M-10 docks with Mir's extreme forward port.
----------------------------------------------------------------------------
 1992.
----------------------------------------------------------------------------
20 JAN    Progress M-10 undocks and is directed into the atmosphere to
          burn-up. Recoverable capsule re-enters.
25 JAN    Progress M-11 launched.
27 JAN    Progress M-11 docks with Mir's extreme forward port.
20 FEB    Volkov and Krikalyov make a 4 hour, 12 minute spacewalk to
          install and retrieve instruments. Objectives curtailed by Volkov's
          spacesuit malfunction.
13 MAR    Progress M-11 undocks and is directed into the atmosphere to
          bur-up.
14 MAR    Soyuz TM-13 transfered to Mir's extreme forward port by Volkov
          and Krikalyov.
17 MAR    Soyuz TM-14 launched with Alexsandr Viktorenko, Alexsandr Kaleri,
          and Klause-Dietritch Flade (Germany) aboard.
19 MAR    Soyuz TM-14 docks with Kvant-1's rear port.
25 MAR    Soyuz TM-13 undocks and re-enters with Volkov, Krikalyov and
          Flade aboard.
19 APR    Progress M-12 launched.
?? APR    Progress M-12 docks with Mir's extreme forward port.
27 JUN    Progress M-12 undocks and is directed into the atmosphere to
          burn-up.
30 JUN    Progress M-13 launched.
02 JUL    Progress M-13 unsuccesfull in docking attempt.
04 JUL    Progress M-13 docks with Mir's extreme forward port.
-----------------------------------------------------------------------------
-----------------------------------------------------------------------------
 
    N.B  This diary lists all events up until 4 JUL 92. I am quite certain
        that I have included all launches, dockings, spacewalks, and
        re-entries. The only important events that I am not sure of are
        launchings of micro-satellites (if any) that may have taken place
        from Mir's airlocks. I would be grateful to anyone who can tell
        me of such events.

                          Bye for now Tim.
 
225.23MIR Mission Chronicle 9VERGA::KLAESI, RobotWed Dec 16 1992 19:1184
From:	DECWRL::"vsa@msd.orbi.kostroma.su" "Voevodin S.A." 15-DEC-1992 
To:	mcdowell@urania.harvard.edu
Subj:	VSA034: The 9th Mir Mission Chronicle

    ***********************************************************
    *  VSA034       13.12.1992       (c) Sergey  A. Voevodin  *
    ***********************************************************

    MISSION CHRONICLE  No 7
    ~~~~~~~~~~~~~~~~~

                Mir: the 9th Resident Mission

    Soyuz TM-12     L    18.05.91      11:50:28   GMT
                    D    20.05.91      13:50:43   GMT
                    UD   23.05.91      10:10:??   GMT
                    RD   23.05.91      10:52:??   GMT
                    UD   10.10.91      00:55:08   GMT
                    B    10.10.91      03:16:14   GMT
                    LD   10.10.91      04:12:18   GMT

           eject MAK-1   17.06.91      02:58:??   GMT
            satellite

                    Duration:  Artsebarsky         144d 15h 21m 50s
                               Aubakirov/Flade       7d 22h 12m 39s


    Progress M-8    L    30.05.91      08:04:??   GMT
                    D    01.06.91      00:45:??   GMT
                    UD   15.08.91      22:17:??   GMT
                    B    16.08.91      ??:??:??   GMT


    Progress M-9    L    20.08.91      22:54:??   GMT
                    D    23.08.91      00:54:??   GMT
                    UD   30.09.91      01:54:??   GMT
                    B    30.09.91      ??:??:??   GMT
                    LCE  30.09.91      ??:??:??   GMT
                    LD   30.09.91      08:18:??


    Soyuz TM-13     L    02.10.91      05:59:39   GMT
                    D    04.10.91      07:38:42   GMT

                    Artsebarsky/Krikalyov EVAs:

             1. 24.06.91   hatch open   - 21:11:??  GMT
                25.06.91         close  - 02:09:??  GMT

                           EVA duration -  4h 58m

                           replace the Kurs docking system antenna

             2. 28.06.91   hatch open   - 19:02:??  GMT
                                 close  - 22:26:??  GMT

                           EVA duration -  3h 24m

                           install TREK equipment

             3. 15.07.91   EVA duration -  5h 45m

             4. 19.07.91   hatch open   - 11:10:??  GMT
                                 close  - 16:38:??  GMT

                           EVA duration -  5h 28m

             5. 23.07.91   hatch open   - 09:16:??  GMT
                                 close  - 14:50:??  GMT

                           EVA duration -  5h 34m

             6. 27.07.91   EVA duration -  6h 49m

                           install "Sofora" girder

    Abbreviation: L - launch; D - docking; UD - undocking; RD - redocking;
                  B - TDU-burn; LCE - landing capsule ejection; LD - landing;
                  DS - destruction

% ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ======
% From: vsa@msd.orbi.kostroma.su (Voevodin S.A.)

225.24MIR Mission Chronicle 10VERGA::KLAESI, RobotWed Dec 16 1992 19:1169
From:	DECWRL::"vsa@msd.orbi.kostroma.su" "MAIL-11 Daemon" 9-DEC-1992 
To:	sci-space-news@ames.arc.nasa.gov
CC:	
Subj:	VSA030: 10th Mir Resident Mission Chronicle

    ***********************************************************
    *  VSA030       07.12.1992       (c) Sergey  A. Voevodin  *
    ***********************************************************

    MISSION CHRONICLE  No 5
    ~~~~~~~~~~~~~~~~~

                Mir: the 10th Resident Mission

     Soyuz TM-13     L    02.10.91      05:59:39   GMT
                     D    04.10.91      07:38:42   GMT
                     UD   15.10.91      01:01:??   GMT
                     RD   15.10.91      02:45:??   GMT
                     UD   14.03.92      11:43:??   GMT
                     RD   14.03.92      12:10:??   GMT
                     UD   25.03.92      05:26:??   GMT
                     B    25.03.92      07:55:??   GMT
                     LD   25.03.92      08:51:22   GMT

                     Duration:  Volkov        175d 02h 52m 43s
                                Krikalyov     311d 20h 01m 54s
                                Flade           7d 21h 57m 52s


     Progress M-10   L    17.10.91      00:05:??   GMT
                     D    19.10.91     (02:15)     unsuccessful
                     D    21.10.91     (02:02)     unsuccessful
                     D    21.10.91      03:40:50   GMT
                     UD   20.01.92      07:14:??   GMT
                     B    20.01.92      ??:??:??   GMT
                     LCE  20.01.92      ??:??:??   GMT
                     LD   20.01.92      12:06:??   GMT


     Progress M-11   L    25.01.92      07:50:??   GMT
                     D    27.01.92      09:31:??   GMT
                     UD   13.03.92      09:43:40   GMT
                     B    13.03.92      ??:??:??   GMT
                     DS   13.03.92      16:47:46   GMT


     Soyuz TM-14     L    17.03.92      10:54:30   GMT
                     D    19.03.92      12:32:50   GMT


                     Volkov/Krikalyov EVAs:

                20.02.92   hatch open   - 20:09:20  GMT
                21.02.92         close  - 00:21:??  GMT

                           EVA duration -  4h 12m

                           dismantle of "Sofora" subsidary units
                           install "Danko-M"
                           return "Sprut-5"

Abbreviation: L - launch; D - docking; UD - undocking; RD - redocking;
              B - TDU-burn; LCE - landing capsule ejection; LD - landing;
              DS - destruction

% ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ======
% From: vsa@msd.orbi.kostroma.su (Voevodin S.A.)
% Subject: VSA030: 10th Mir Resident Mission Chronicle

225.25MIR Mission Chronicle 11VERGA::KLAESI, RobotWed Dec 16 1992 19:1256
From:	DECWRL::"vsa@msd.orbi.kostroma.su" "Voevodin S.A." 10-DEC-1992 
To:	Radley@nss.org
Subj:	VSA031: The 11th Mir Resident Mission Chronicle

   ***********************************************************
   *  VSA031       09.12.1992       (c) Sergey  A. Voevodin  *
   ***********************************************************

    MISSION CHRONICLE  No 6
    ~~~~~~~~~~~~~~~~~

                 Mir: the 11th Resident Mission

   Soyuz TM-14     L    17.03.92      10:54:30   GMT
                   D    19.03.92      12:32:50   GMT
                   UD   09.08.92      21:46:47   GMT
                   B    09.08.92      ??:??:??   GMT
                   LD   10.08.92      01:05:02   GMT

                   Duration:  Viktorenko/Kalery   145d 14h 10m 32s
                              Tognini              13d 18h 56m 14s


   Progress M-12   L    19.04.92      22:29:??   GMT
                   D    22.04.92      00:22:??   GMT
                   UD   27.06.92      22:35:??   GMT
                   B    28.06.92      ??:??:??   GMT


   Progress M-13   L    30.06.92      16:43:??   GMT
                   D    02.07.92     (17:25)     GMT   unsuccessful
                   D    04.07.92      16:55:??   GMT
                   UD   24.07.92      03:14:??   GMT
                   B    24.07.92      ??:??:??   GMT


   Soyuz TM-15     L    27.07.92      06:08:48   GMT
                   D    29.07.92      07:46:??   GMT

                   Viktorenko/Kalery EVA:

                   08.07.92   hatch open   - 11:37:41  GMT
                   21.02.92         close  - 13:41:??  GMT

                              EVA duration -  2h 03m

                              install an valve for vacuumation of gyrodynes

   Abbreviation: L - launch; D - docking; UD - undocking; RD - redocking;
                 B - TDU-burn; LCE - landing capsule ejection; LD - landing;
                 DS - destruction

% ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ======
% From: vsa@msd.orbi.kostroma.su (Voevodin S.A.)
% Subject: VSA031: The 11th Mir Resident Mission Chronicle

225.26MIR Mission Chronicles 1-3VERGA::KLAESI, RobotThu Dec 31 1992 14:57186
Article: 2732
Newsgroups: sci.space.news
From: vsa@msd.orbi.kostroma.su (Voevodin S.A.)
Subject: From VSA archives
Sender: news-service@newcom.kiae.su
Organization: AO ORBI (MS-DOS)
Date: Mon, 21 Dec 1992 12:57:04 GMT
 
( Mission Chronicle No 1 )
 
              5th Resident Expedition Chronicle

 
Soyuz TM-8    Launch (L)       05.09.89     20:38:03   UT
              Docking (D)      07.09.89     21:25:26   UT
              Undocking (U)    12.12.89     07:22:30   UT
              Redocking (RD)   12.12.89     07:42:32   UT
              U                19.02.90     00:06:20   UT
              Landing (LD)     19.02.90     03:36:18   UT
 
 
Viktorenko & Serebrov duration     166:06:58:15
 
 
Progress M    L                23.08.89     02:09:32   UT
              D                25.08.89     04:19:01   UT
              U                01.12.89     08:02:23   UT
              TDR-Burn (T)     01.12.89     09:32:00   UT
 
 
Kvant-2       L                26.11.89     12:01:41   UT
              D                06.12.89     11:21:28   UT
              U                08.12.89     06:19:07   UT
              RD to Top port   08.12.89     07:19:04   UT
 
 
Progress M-2  L                20.12.89     02:30:50   UT
              D                22.12.89     04:41:21   UT
              U                09.02.90     01:33:07   UT
              T                09.02.90     06:07:00   UT
 
 
Soyuz TM-9    L                11.02.90     05:16:00   UT
              D                13.02.90     05:37:47   UT
 
 
        Viktorenko/Serebrov EVAs:
 
1. 08.01.90     open - 19:23                closed - 22:19
                through Bottom Mir docking port
                Installed: 2 star detectors (80 kg each)
                Returned: Meduza units
 
2. 11.01.90     open - 17:01                closed - 19:55
                through Bottom Mir docking port
                Istalled: ARFA-E electrones injector
                Returned: Enchallone & ERA (France)
                Repaired Bottom Mir docking port for Kristall
 
3. 26.01.90     open - 11:09                closed - 14:11
                through Special Kvant-2 Hatch (SH)
                Tested: Orlan-DMA spacesuits
                Installed: special EVA units for SPK docking,
                           TV platform,
                           Ferrit & Danko units,
                           Etalon-D & Plyonka-3 cassetes.
                Returned: Kurs antennas.
 
4. 01.02.90     open - 07:15                closed - 12:14
                through SH
                Serebrov tested SPK ( 33 m distance )
 
5. 05.02.90     open - 05:08                closed - 08:53
                through SH
                Viktorenko tested SPK ( 45 m distance )
                Measured radiation near Mir station using
                SPIN-6000 spectrometre
 
 <c> VSA. 1990                                      22.10.90
 
------------------------------------------------------------
 
( Mission Chronicle No 2 )
 
*****************************************************************
*  VSA008       31.01.1991       (c) Sergey  A. Voevodin. 1991  *
*****************************************************************
 
 
               6th Resident Mission to Mir Chronicle
 
 
Soyuz TM-9    Launch (L)      11.02.90     05:16:00   UT
              Docking (D)     13.02.90     05:37:47   UT
              Undocking (U)   21.02.90     02:56:01   UT
              Redocking (R)   21.02.90     03:15:23   UT
              U               28.05.90     10:45:13   UT
              R               28.05.90     11:11:17   UT
              U               03.07.90     21:07:04   UT
              R               03.07.90     21:31:12   UT
              U               09.08.90     03:08:49   UT
              Landing         09.08.90     06:33:57   UT
 
 
Soyuz TM-8    U               19.02.90     00:06:20   UT
              Landing         19.02.90     03:36:18   UT
 
 
Progress M-3  L               28.02.90     22:10:57   UT
              D               03.03.90     00:05:11   UT
              U               26.04.90     19:24:23   UT
              TDR-Burn (T)    26.04.90     23:00:00   UT
 
 
Progress-42   L               05.05.90     19:44:01   UT
              D               07.05.90     21:45:13   UT
              U               27.05.90     06:08:58   UT
              T               27.05.90     10:40:00   UT
 
 
Kristall      L               31.05.90     09:33:20   UT
              D               10.06.90     09:47:22   UT
              U               11.06.90     ??:??:??   UT
              R               11.06.90     ??:??:??   UT
 
 
              Soloviyov/Balandin EVAs:
 
 
 17.07.90      open - 12:06             closed - 19:06
               Repair of thermoisolation
 
 26.07.90      open - 10:15             closed - 13:46
               Hidding of repair units & repair of the hatch.
 
 
-----------------------------------------------------------------
 
( Mission Chronicle No 3 )
 
 
*****************************************************************
*  VSA013       01.06.1991       (c) Sergey  A. Voevodin. 1991  *
*****************************************************************
 
 
             7th resident Mission on Mir Chronicle
 
 
Soyuz TM-10    Launch (L)      01.08.90        08:32:21   UT
               Docking (D)     03.08.90        10:45:44   UT
               Undocking (UD)  10.12.90        01:48:11   UT
               Landing (LD)    10.12.90        05:08:12   UT
 
 
Manakov & Strekalov duration  - 130 d 20 h 35 m 51 s
Akiyama duration              -   7 d 21 h 54 m 40 s
 
 
Soyuz TM-9     U               09.08.90        03:08:49   UT
               LD              09.08.90        06:33:57   UT
 
 
Progress M-4   L               15.08.90        03:00:41   UT
               D               17.08.90        04:26:15   UT
               UD              17.09.90        11:42:43   UT
               TDR             20.09.90        10:04:27   UT
 
 
Progress M-5   L               27.09.90        09:37:42   UT
               D               29.07.90        11:26:51   UT
               UD              28.11.90        05:15:16   UT
               TDR             28.11.90        09:24:28   UT
               Landing capsule
               ejection (LCE)  28.11.90        09:49:47   UT
 
 
Soyuz TM-11    L               02.12.90        07:13:32   UT
               D               04.12.90        08:57:09   UT
 
 
                     Manakov/Strekalov EVA
 
29.10.90        open - 20:45                 close - 23:30
                repair of the hatch
 
225.27The MIR lavatoryVERGA::KLAESQuo vadimus?Fri Sep 10 1993 17:0452
Article: 14997
Newsgroups: sci.space.shuttle
From: ghasting@vdoe386.vak12ed.edu (George Hastings)
Subject: Re: Toilet Question
Organization: Virginia's Public Education Network (Richmond)
Date: Fri, 10 Sep 93 01:41:45 GMT
 
Another followup to the previous... on a more serious note, I promise!
 
	The toilet system aboard the russian MIR is very similar to
the new toilet system on shuttles. The facility itself LOOKs quite a
bit different: more like a regular toilet. A lock-down lever is
lifted, revealing a small, slightly saddle-shaped opening. The toilet
itself is small enough to straddle. There are some other differences:
before using the MIR toilet, something sort of like a non-woven cloth
vacuum-cleaner bag is placed in a holder which keeps it open, and that
in turn is placed in the toilet opening. Small holes around the edge
of the toilet admit air to provide an airflow into this bag and
through it as it is being used, pulling feces into the bag. Urine
passes through the bag walls and is later vented overboard. 

	After the toilet paper is used and is pulled into the bag, the
cosmonaut floats off the facility, and reaching toward it, pulls two
protruding rubber-band-like tabs. Rigid trap-door like covers snap
from the edges of the bag insert, closing it effectively. The vacuum
system is then turned off, and the cosmonaut removes the used bag,
inserts it into a plastic bag, and carries it out the oval door of the
bathroom facility. Just around the corner in the wardroom area, a part
of the floor has a trapdoor section about .75M x 1.0M, if I remember
correctly. Opening this, the one door of the garbage-disposal airlock
is revealed. Opening THAT, the fecal-containment bag is placed inside,
and both doors are closed. 

   Eventually when the garbage containment bag in that airlock is full
of human and other waste such as food-wrappers, etc., the outside
airlock is opened, and the package jettisoned in a direction
retrograde to the path of MIR. Eventually, losing altitude, it burns
up as it re-enters the atmosphere. 

  Just think: the next time you look up at a clear night sky and see a
brief streak of blazing light zipping across a few degrees of sky
before disappearing, it MIGHT not be a meteor. You MAY be watching
flaming....THINGS!!!! 8-) 

 ____________________________________________________________
| George Hastings		ghasting@vdoe386.vak12ed.edu |  
| Space Science Teacher		72407.22@compuserve.com      |If it's not
| Mathematics & Science Center 	STAREACH BBS: 804-343-6533   | FUN, it's
| 2304 Hartman Street		OFFICE:       804-343-6525   |probably not
| Richmond, VA 23223		FAX:          804-343-6529   |  SCIENCE!
 ------------------------------------------------------------

225.28Supplying MIRVERGA::KLAESQuo vadimus?Wed Sep 15 1993 19:31216
Article: 70112
Newsgroups: sci.space
From: dennisn@ecs.comm.mot.com (Dennis Newkirk)
Subject: Re: Russian Resupply 
Organization: Motorola
Date: Mon, 23 Aug 1993 15:53:27 GMT
Sender: news@lmpsbbs.comm.mot.com (Net News)
 
In article <259d6eINN1ei@lynx.unm.edu> butina@netsun.mdc.com (Tony Butina) 
writes: 

>I heard an interesting bit regarding Russian MIR resupply.  It seems to be
>a one way trip.  Build cheap hardware and when if fails throw it overboard
>and send up replacement units only.  Just resupply and no return.  Anyone
 
Return of material from Mir is the weakest link in the Mir transport
system. This is mostly the result of the program using equipment
originally designed in the 1960's to fly cosmonauts around the moon.
Returning much payload is not required for that mission. In the late
1960's as space station projects like Almaz and Salyut started in the
USSR the Soyuz was the newest manned transport spacecraft available
and it was adopted by both projects to service space stations. Funding
constraints and schedule seem to have been major factors in this
decision. Thus, todays Soyuz TM still has limited return payload mass
and volume, although new designs have been on the drawing boards for
many years. Usually only experiment results are returned such as film,
processed material, log books, biological samples, etc., about 100-150
kg. worth and only when crews are exchanged which is about every 6
months. The Progress also can carry a small return capsule and this is
sometimes used to return about the same ammount. 
 
Chief Designer Chelomie did have a new manned transport design to use
with his Almaz military space station but it was delayed for many
years and eventually flew as space station modules (Kosmos 929, 1256,
etc..). It was was reportedly only used once to return payload from
Salyut 7. Continued use of the module for transport missions was ended
due to its use of the Proton which was more expensive than a Soyuz
booster, and the fact that it was designed and built by rival firms to
the main manned spaceflight organization, NPO Energia. The Buran of
course solves the problem of return payload capacity but
realisticially would only be needed a few times a year at most, and
its high cost makes it very uneconomical. The perfect solution would
be for a NASA shuttle to dock to Mir periodicially and make a pick-up
of any payloads needing return. So far there seems to be little need
for this service since the Russian stations have operated without it
for many years. But, there's nothing stopping anyone from hiring the
Russians to launch an experiment to Mir and hiring NASA to retreive
it. It's unclear if the Russians consider such a service useful. If
they did, it would seem to open the way to more cooperation with the
Russians launching NASA experiments to Mir and NASA retreiving Russian
materials with the shuttle. The 1995 NASA Mir mission and the
shuttle-Mir docking mission will demonstrate this. It is reportedly
hoped by some at NASA that such missions will continue in the future. 
 
Dennis Newkirk (dennisn@ecs.comm.mot.com)
Motorola, Land Mobile Products Sector
Schaumburg, IL

Article: 70165
Newsgroups: sci.space
Subject: Re: Russian resupply
From: charles.radley@pcohio.com (Charles Radley)
Date: Mon, 23 Aug 93 18:34:00 -0500
Organization: PC-OHIO PCBOARD - Cleveland, OH - 216-381-3320
 
 -=> Quoting Allen W. Sherzer to All <=-
 
 >I heard an interesting bit regarding Russian MIR resupply.  It seems to be
 >a one way trip.  Build cheap hardware and when if fails throw it overboard
 >and send up replacement units only.  Just resupply and no return.  Anyone
 
 AWS> I don't have the details handy, but the Russians make a range of cargo
 AWS> return vehicles which return from a few hundered to a few thousand
 AWS> pounds of cargo.
 
Unfortunately no, Allen.   The Progress resupply vehicles cannot
return to Earth, they are re-entered over the Pacific. 
 
The Soyuz manned capsules have very little cargo return capability,
the "Orbital Module" front section is jetissoned before re-entry, and
the crew cabin is very cramped.   No storage lockers to speak of. 
 
I have heard stories of cosmonauts holding crystal samples between
their knees during re-entry. 
 
The Russians have some tiny re-entry capsules which are ejected from
the Mir airlock.  They are not used very often, and one of them was
lost somewhere in the Urals with a full load of samples. 
 
One of the major benefits of a Shuttle visit to Mir is that large
masses of samples can be returned to Earth from Mir. I suspect there
are lots of crystal samples "marrooned" on Mir because of lack of
return capacity to Earth. 
 
.... Internet address:- DJ320@CLEVELAND.FREENET.EDU  Ad Astra per Guile !
--- Blue Wave/QWK v2.10

Article: 70175
From: gwh@soda.berkeley.edu (George William Herbert)
Newsgroups: sci.space
Subject: Re: Russian resupply
Date: 24 Aug 1993 01:22:39 GMT
Organization: Retro Aerospace
 
In article <24.13999.1898.0NB2A21F@pcohio.com>,
Charles Radley <charles.radley@pcohio.com> wrote:

>The Russians have some tiny re-entry capsules which are ejected
>from the Mir airlock.  They are not used very often, and one of
>them was lost somewhere in the Urals with a full load of samples.
 
They also have a small capsule which is carried partway down (deorbit
burn, but not re-entry) inside a Progress, then seperated later to
re-enter intact and seperately. 
 
They've been pushing a series of similar re-entry capsules. For
instance, the one they're selling to the Germans to use in an ESA (?)
experiment.  Rumor is that some of these reentry vehicles are just
that; old ICBM RV designs. 
 
-george william herbert
Retro Aerospace
 
Article: 70330
Newsgroups: sci.space
From: dennisn@ecs.comm.mot.com (Dennis Newkirk)
Subject: Re: Russian resupply
Organization: Motorola
Date: Tue, 24 Aug 1993 22:29:57 GMT
Sender: news@lmpsbbs.comm.mot.com (Net News)
 
In article <24.13999.1898.0NB2A21F@pcohio.com>
charles.radley@pcohio.com (Charles Radley) writes: 

>....The Progress resupply vehicles cannot return to
>Earth, they are re-entered over the Pacific.
 
 Some Progress-M are equipped with return capsules. They replace the 
 docking probe and are jettisoned after retrofire. They are about
 a meter long and .5 meters in diameter widening to the hatch 
 diameter at one end. In this case the Progress does not make it
 to the Pacific. These capsules can return 100-150 kg.. 
 
>The Soyuz manned capsules have very little cargo return capability,
>the "Orbital Module" front section is jetissoned before re-entry, and
>the crew cabin is very cramped.   No storage lockers to speak of.
>I have heard stories of cosmonauts holding crystal samples between
>their knees during re-entry.
 
 I do NOT speak from experience of crawling around in a Soyuz, but I 
 suspect there may be some room under the seats, and there is room around 
 the orbital module hatch if their brave enough to use it. Capsules 
 with 2 cosmonauts are not as cramped as with 3 and in those
 cases there is enough room for payload volume and mass to equal
 a human and a seat. It may not be as easy to use as a storage locker
 but I'm sure lashing items to the capsule wall is effective.
  
 As I stated in an earlier post the Soyuz TM is supposed to have a 
 100-150 kg. return payload. This is much improved from the days
 of the Soyuz of the 1970's which had only 50 kg. return payload.
 
>The Russians have some tiny re-entry capsules which are ejected
>from the Mir airlock.  They are not used very often, and one of
>them was lost somewhere in the Urals with a full load of samples.
 
 You mean Progress return capsules. Mir has ejected satellites 
 from airlocks but not return capsules. They would have to be VERY 
 small and include retro rockets, etc.... The old Salyut 3 and 5
 had 1-2 small capsules for film/sample return. Some cosmonauts
 have low reguard for the bumpy landing the small capsules make.
 I don't know if they've attempted air intercepts but it would
 seem to be a good idea.
 
>One of the major benefits of a Shuttle visit to Mir is that 
>large masses of samples can be returned to Earth from Mir.
>I suspect there are lots of crystal samples "marrooned" on
>Mir because of lack of return capacity to Earth.
 
 From reading cosmonauts complaints it's not lack of returned
 results, but lack of follow-up on the ground once the results
 are in hand. At least a few cosmonauts have made this complaint.
 
 The Russians could launch an unmanned Soyuz and fill the entire
 capsule with results if needed.
 
 Dennis Newkirk (dennisn@ecs.comm.mot.com)
 Motorola, Land Mobile Products Sector
 Schaumburg, IL

Article: 71309
Newsgroups: sci.space
From: kjenks@gothamcity.jsc.nasa.gov
Subject: Re: Russian Resupply
Sender: usenet@aio.jsc.nasa.gov (USENET News Client)
Organization: NASA/JSC/DE44, Mission Operations, Space Station Systems 
Date: Mon, 30 Aug 1993 21:55:02 GMT
 
Tony Butina (butina@netsun.mdc.com) wrote:
 
: I heard an interesting bit regarding Russian MIR resupply.  It seems to be
: a one way trip.  Build cheap hardware and when if fails throw it overboard
: and send up replacement units only.  Just resupply and no return.  Anyone
: hear anything about this, confirm or deny?
 
That's what I hear through the rumor mill.  Evidently, Mir is getting
awfully crowded with stuff.  Although early pictures showed lots of
habitable volume, these days there's rumored to be just a small
corridor down the middle of the big module, with various pieces of
equipment attached piecemeal all over the inside of the place.
 
-- Ken Jenks, NASA/JSC/DE44, Mission Operations, Space Station Systems
      kjenks@gothamcity.jsc.nasa.gov  (713) 483-4368
 
     "The Earth is the cradle of humanity, but mankind will not stay in
     the cradle forever." -- Konstantin Tsiolkvosky

225.29Some MIR modules derived from U.S. MOLVERGA::KLAESQuo vadimus?Thu Sep 16 1993 19:3042
Article: 72793
From: David.Anderman@ofa123.fidonet.org
Newsgroups: sci.space
Subject: Re: MOL
Date: 16 Sep 93 23:00:37 GMT
 
 -=> Quoting Gary Coffman to All <=-
 
 GC> In article <32022@ksr.com> clj@ksr.com (Chris Jones) writes:
 >In article <1993Sep12.162724.20497@ke4zv.atl.ga.us>, gary@ke4zv (Gary
  Coffman)
 GC> writes: >>MOL eventually got transformed into Big Bird, the monster
 GC> unmanned >>spy satellite. MOL was a cover for a manned spy satellite. 
 
Well, the problem with this theory is that MOL was built by MacDac at
its Huntington Beach, California plant, whereas the Big Birds were
built either by Lockheed or TRW elsewhere. I presume that whoever is
building spy sats like Bird Bird and its successors is still building
them in the same place as Big Bird, whereas the MOL construction
facility is clearly no longer being used for large satellites like
MOL; rather it is being used as a construction hangar for the DC-X. 
 
Furthermore, MOL was a 10 foot diameter vehicle, but the large spysats
are launched in 15 foot diameter fairings. 
 
It is fairly obvious that MOL was cancelled in favor of the later Big
Bird, but was a separate program. Perhaps some MOL technology went
into unmanned spysats. 
 
Interestingly, the Soviets copied MOL as they copied many Western
military systems. Their version was called the "Star" module, and
featured a Gemini-style spacecraft to be launched on top of the stack.
Cosmonauts would transfer from the capsule to the Star module via a
hatch in the heat shield. 
 
These Star modules (now minus the Gemini-type capsule) are still in
use in the Russian manned space station. One version is called the
Kristall; others to be launched are called Priroda and Spektr. 
 
.... Open mouth, insert foot, echo internationally.
--- Blue Wave/Max v2.12 [NR]

225.30RE 225.29VERGA::KLAESQuo vadimus?Fri Sep 17 1993 20:08112
Article: 72900
Newsgroups: sci.space
From: dennisn@ecs.comm.mot.com ()
Subject: Re: MOL
Organization: Motorola
Date: Thu, 16 Sep 1993 16:57:20 GMT
Sender: news@lmpsbbs.comm.mot.com (Net News)
 
In article <5515939d8@ofa123.fidonet.org>,
David.Anderman@ofa123.fidonet.org writes: 

> Interestingly, the Soviets copied MOL as they copied many Western
> military systems. Their version was called the "Star" module, and
> featured a Gemini-style spacecraft to be launched on top of the
> stack. Cosmonauts would transfer from the capsule to the Star
> module via a hatch in the heat shield.  
 
Close but not right. Star Modules (TKS - Transport Craft of Supply)
were only to be manned transports to Almaz military space stations
(Salyut 2, 3, 5). The Almaz station had the major instruments,
cameras, and return capslue, it was even proposed once that it have a
gun for self defence. The TKS was a big manned transport with plenty
of room for cargo for a long mission, and add additional propulsion
and power to the Almaz station when docked. 
 
The Almaz was the first (acknowledged) Soviet space station program.
Everything was new about the design and Chief Designer Chelomey was
given the project. In 1969 the Korolev KB got a project to use
Chelomey's Almaz hull as the basis of a space station that was
outfitted with Soyuz components (propulsion, life support, control,
guidance, etc..) and this became the civilian Salyut. The Almaz
booster, the Proton, was also used by the Korolev KB since it was
already developed as part of the manned circumlunar project.... 
 
The Korolev program bounded far ahead of the Almaz project due to its
use of already developed Soyuz technology and was ready for flight in
1971. The Korolev bureau also planned to use a version of its Soyuz
lunar spacecraft as a manned transport to the new Salyut station, and
resulted in the Salyut 1/Soyuz 10 and 11 missions. 
 
Meanwhile, back at the Chelomey bureau, Almaz problems, funding
problems or political problems meant that the TKS would have to be
delayed indefinitely and Chelomey was forced to use the only
alternative manned transport which was the Korolev Soyuz. Thus we saw
the Salyut 3/Soyuz 14 in 1974, etc... Finially in 1977 a complete TKS
was flown for the first time, was later used as a supply module for
Salyut 6 & 7 (Kosmos 1256, 1443, 1669, 1686). Up until the 1980's it
still could have been used as a manned transport to the second
generation military Almaz stations which were never launched due to
weight problems and limitations of the Proton booster. Now the TKS is
highly modified to serve as Mir modules. Space News even states that
NASA is interested in the TKS propulsion system for the NASA space
station. 
 
Test flights of the TKS capsule account for the once mysterious dual
Kosmos missions 881/882, 997/998, etc... Apparently the Kosmos 1443
capsule is up for auction in December. 
 
The real question you all probably have is, why does the TKS exist if
a Soyuz will do the job? Well, in part Chelomey was given the Almaz
project and he wanted to keep all the development to his organization,
the Proton, Almaz and TKS (which required a Proton - how convienient
to keep those production lines open...). There were probably some
reasons the TKS had to be as big as it was and maybe some political
and military reasons to have a system seperate from Korolev's Soyuz
and its booster, etc... Time will tell..... 
 
Dennis Newkirk (dennisn@ecs.comm.mot.com)
Motorola, Land Mobile Products Sector
Schaumburg, IL

Article: 72925
Newsgroups: sci.space
From: gary@ke4zv.atl.ga.us (Gary Coffman)
Subject: Re: MOL
Organization: Destructive Testing Systems
Date: Thu, 16 Sep 1993 21:44:34 GMT
 
In article <5515939d8@ofa123.fidonet.org>
David.Anderman@ofa123.fidonet.org writes: 

> -=> Quoting Gary Coffman to All <=-
>
> GC> In article <32022@ksr.com> clj@ksr.com (Chris Jones) writes:
> >In article <1993Sep12.162724.20497@ke4zv.atl.ga.us>, gary@ke4zv (Gary
>Coffman)
> GC> writes: >>MOL eventually got transformed into Big Bird, the monster
> GC> unmanned >>spy satellite. MOL was a cover for a manned spy satellite. 
> 
>Well, the problem with this theory is that MOL was built by
>MacDac at its Huntington Beach, California plant, whereas the
>Big Birds were built either by Lockheed or TRW elsewhere. I
>presume that whoever is building spy sats like Bird Bird and its
>successors is still building them in the same place as Big Bird,
>whereas the MOL construction facility is clearly no longer being
>used for large satellites like MOL; rather it is being used
>as a construction hangar for the DC-X.
 
The MOL and Big Bird were built by the Air Force. The contractors they
used are irrelevant to this discussion. According to _Deep Black_,
both projects were based on the same 54 foot Agena profile, both used
the same 6 foot diameter telescope, both had the same mission, etc.
Obviously, the manned version was much different internally from the
eventually flown automated spysat version. 
 
Gary
-- 
Gary Coffman KE4ZV          |"If 10% is good enough | gatech!wa4mei!ke4zv!gary
Destructive Testing Systems | for Jesus, it's good  | uunet!rsiatl!ke4zv!gary
534 Shannon Way             | enough for Uncle Sam."| emory!kd4nc!ke4zv!gary 
Lawrenceville, GA 30244     | -Ray Stevens          | 

225.31MIR orbit altitudesVERGA::KLAESQuo vadimus?Thu Dec 16 1993 18:3869
From:	US1RMC::"kd2bd@ka2qhd.de.com" "John Magliacane" 16-DEC-1993 10:25:30.91
To:	usenet-space-news@arc.nasa.gov
CC:	
Subj:	* SpaceNews 13-Dec-93 *

SB NEWS @ AMSAT $SPC1213
* SpaceNews 13-Dec-93 *
 
BID: $SPC1213
 
                               =========
                               SpaceNews
                               =========
 
                         MONDAY DECEMBER 13, 1993
 
SpaceNews originates at KD2BD in Wall Township, New Jersey, USA.  It is
published every week and is made available for unlimited distribution.
 
* MIR NEWS *
============
Jean-Claude, FB1RCI, of Marseille, France has provided a graphical view
depicting the altitude of the Russian space station Mir over the past year
based on the mean motion of the spacecraft:
 
Rev per day
 
 
15.53                     I\_
                          I  \_
15.55                     I    \_
                          I      \__                                 _
                   _      I         \__        _     __         I\  I
                  I \_    I            \___   I \_  I  \___     I \ I
15.60 _       _   I   \_  I                \__I   \_I      \____I  \I
       \_    I \_ I     \/                               
         \_  I   \I
           \_I
15.65
 
     /\______________________________/\_________________________________/\__
     1992                           1993                               1994
 
                       (I = Boost to higher orbit)
  
* FEEDBACK/INPUT WELCOMED *
===========================
Mail to SpaceNews should be directed to the editor (John, KD2BD) via any
of the following paths:
 
FAX      : 1-908-747-7107
PACKET   : KD2BD @ N2KZH.NJ.USA.NA
INTERNET : kd2bd@ka2qhd.ocpt.ccur.com  -or- kd2bd@amsat.org
 
MAIL     : John A. Magliacane, KD2BD
           Department of Engineering and Technology
           Advanced Technology Center
           Brookdale Community College
           Lincroft, New Jersey  07738
           U.S.A.
 
       <<=- SpaceNews: The first amateur newsletter read in space! -=>> 
 
--
John A. Magliacane, KD2BD   * /\/\ * Voice   : 1-908-224-2948
Advanced Technology Center  |/\/\/\| Packet  : KD2BD @ N2KZH.NJ.USA.NA
Brookdale Community College |\/\/\/| Internet: kd2bd@ka2qhd.ocpt.ccur.com
Lincroft, NJ  07738         * \/\/ * Morse   : -.-  -..  ..---  -...  -..

225.32BBC program featuring MIR activitiesVERGA::KLAESQuo vadimus?Thu Dec 23 1993 17:1694
Article: 80062
Organization: mbp IT GmbH at ESOC, Darmstadt, Germany
Date: Fri, 17 Dec 1993 14:36:02 CET
From: Dr. Lutz Massonne <LMASSONN@ESOC.BITNET>
Newsgroups: sci.space
Subject: Re: Flames in space (real, not email!)
 
Just yesterday the German TV aired a lengthy (BBC) documentary about
the ex-Soviet space program and they had some footage from aboard the
Mir space station. 

In one scene, the cosmonauts were at first playing with a small car
model which they pushed across a table (and when the table ended, the
car proceeded to run straight ahead) and then, one cosmonaut got a box
of matches (!) and lighted one, letting it drift around inside MIR. At
first, the match did move straight, rotating slowly, and the flame had
a globular appearance. Then, the match seemed to enter the air stream
of some ventilation equipment, it moved faster and the flame was
similar to a flame under gravity. 
 
Apart from the interesting fact that life on Mir seems to be much less
regulated than on board the Shuttle (I cannot imagine a Shuttle
astronaut lighting a match), the frequently-occuring question of
flames in space seems to be answered - they exist :-). 
 
I have taped the documentary and will watch the match scene again,
maybe I discover more details 2nd time ... 
 
Regards, Lutz
 
 Dr. Lutz Massonne           - mbp Informationstechnologie GmbH
 Tel. +49 6151 902027        - at ESOC; Robert-Bosch-Str. 5
 Fax  +49 6151 902271        - D-64293 Darmstadt; Germany

Article: 80216
Newsgroups: sci.space,sci.space.policy
From: kjenks@gothamcity.jsc.nasa.gov
Subject: Re: Flames in space (real, not email!)
Sender: usenet@aio.jsc.nasa.gov (USENET News Client)
Organization: NASA/JSC
Date: Mon, 20 Dec 1993 20:04:01 GMT
 
Dr. Lutz Massonne (LMASSONN@ESOC.BITNET) wrote:

: Just yesterday the German TV aired a lengthy (BBC) documentary about
: the ex-Soviet space program and they had some footage from aboard the
: Mir space station.
 
Because of the Apollo 204 fire, NASA is *still* nervous about fire 
in spacecraft.  Similarly, the Russians are *still* nervous about
pressurization accidents after they lost three cosmonauts in 1971
during the Soyuz 11 entry when a pressure relief valve failed,
asphyxiating the crew.  Each of our space agencies has built their
rules based on their own, unique experiences.  When NASA conducts
flammability experiments in space, there are double- or
triple-redundant systems for ensuring that the experiment is safe. 
This is done differently in Russian spacecraft. 
 
We NASA folks cringe at the thought of a *match* in space.
 
-- Ken Jenks, NASA
      kjenks@gothamcity.jsc.nasa.gov  (713) 483-4368
 
                ASCAN (Astronaut Candidate) 10 COMMANDMENTS
     
      1. Keep smiling, but not grinning
 
      2. Keep your humor harmless, pure and perfect.  People don't
         understand irony.
 
      3. Keep your weaknesses to yourself.  If you don't point them out
         to others, they will never see them.
 
      4. Never complain; make survival look easy.
 
      5. You are expected to say something nice after each flight,
         class, of simulation.
 
      6. If you can't say something nice, lie -- nicely.
 
      7. In particular, practice saying, "Thanks for pointing that out,
         sir.  I'll really work on that."
 
      8. Be aggressively humble and dynamically inconspicuous.  Save
         your brilliance for your friends and family.
 
      9. Remember -- whatever's encouraged is mandatory.  Whatever's
         discouraged is prohibited.
 
     10. Nothing is sometimes a good thing to do and always a clever
         thing to say.
 
                             REVIEW THIS LIST DAILY

225.33"Rocket' matches?REPAIR::RICKETTSWell fax meFri Dec 24 1993 06:5716
  On thinking about it, the behaviour of the lighted match is perfectly logical.
The initial globular flame is emitting combustion products (hot gases) equally
in all directions *except* in the direction of the match itself. This imbalance
will inevitably produce a reaction which will push the match away from the
flame. In effect, it will act as a tiny jet engine with a very inefficient
nozzle.
  As it starts to move through the air in the cabin, the airflow will elongate
the flame, causing it to take on a more familiar appearance. The elongation of 
the flame, together with the inflow of air towards it along the match, will also
increase the imbalance in the emission of combustion products, increasing the
thrust.

  NASA's candle experiment involved a candle fixed inside a box, not free to
move through the air, hence this effect was not observed.

Ken
225.34Eight years in Earth orbitVERGA::KLAESQuo vadimus?Mon Feb 21 1994 17:4156
Article: 7027
From: clarinews@clarinet.com (AP)
Newsgroups: clari.world.europe.eastern,clari.news.hot.ussr
Subject: Russia Space Station Lauded
Date: Sun, 20 Feb 94 14:00:07 PST
 
	MOSCOW (AP) -- Three cosmonauts celebrated the eighth
anniversary of the orbiting Russian space station Mir on Sunday,
saying it should instill pride in their countrymen back on Earth. 

	The 130-ton space station was launched by the Soviet Union on
Feb. 20, 1986, and has outlived the country that sent it into space.
Despite turmoil in Russia, including within its space agency, the
aging station has remained an important platform for space research. 

	``We must be proud that the station is still functioning,''
commander Viktor Afanasyev said in a television interview from space. 

	A U.S. space expert expressed admiration for the Mir, which
has circled the globe while America's space station remained on the
drawing board. 

	``It's a treasure trove of experience that must be examined
before we can build a bigger station together,'' said James Oberg, a
senior space engineer and author who follows the Russian program closely. 

	Oberg, speaking in a telephone interview last week from Houston, 
also praised Russia's determination to remain a leader in space. 

	``They have through the coups and the countercoups, through
all the turmoil, they have maintained a manned space platform in
orbit, with continuous occupancy,'' he said. ``This can't be done by
brute force and sheer endurance alone. It requires a high-level,
world-class technology.'' 

	The Mir has been expanded through the years by modules carried
into orbit and has been home to dozens of cosmonauts, some of whom
have spent more than a year aboard -- far longer than any American has
been in space. 

	In March 1995, U.S. astronaut Norman Thagard will rocket into
orbit on a Russian Soyuz and spend three months aboard the Mir with a
Russian crew. Thagard and his backup, Bonnie Dunbar, plan to arrive in
Russia on Thursday to begin training for the mission. 

	Afanasyev and his two crewmates, dressed casually in shorts
for the television interview, paid tribute to the Mir's past and
future occupants. 

	``We are keeping pictures at the station of all the cosmonauts
who worked at it,'' said Valery Polyakov. ``Some of them are not with
us any longer, but we'll always remember them.'' 

	``We congratulate all those who have already worked on the
station, and those who will be working on it,'' said Yuri Usachev. 

225.35MIR Handbook from NPO EnergiaMTWAIN::KLAESKeep Looking UpTue May 03 1994 20:2354
From:	US4RMC::"ssi_mail@espsun.bgm.link.com" 29-APR-1994 16:16:53.21
CC:	
Subj:	NPO Energia: MIR Handbook

NPO ENERGIA LTD

Releases Guides to Products and Services 
and
The MIR 1 Space Station

NPO Energia Ltd. and The Space Business Archive are pleased to
announce the availability of the NPO Energia Guide to Products and
Services and MIR 1 Space Station: A Technical Overview. The first
book, (NPO Energia Guide to Products and Services) is a 172 page
document that has been translated into English from Russian and
includes technical descriptions of equipment and general
specifications for all major NPO Energia programs including the MIR 1
space station, experiment requirements, microgravity, the Energia
launch vehicle, the Soyuz transport spacecraft and the Progress supply
vehicle. The guide also includes information on the engineering and
consulting services available through Energia's team of highly
qualified and respected specialists.  A large array of non-aerospace
products and services are also listed including testing facilities,
promotional services, and consumer products. 

The MIR 1 Space Station: A Technical Overview is a 200 page document
also translated from Russian into English which details lessons
learned, remote sensing, reentry technology, docking systems, mission
control, and MIR 1 experiment requirements. The Overview is based on
the MIR 1 Space Station Sympossium proceedings book. 

This marks the first time in history that a Russian organization, of
NPO Energia's caliber, has made available such an extensive compendium
of its products.  Representatives from NPO Energia, Ltd. will  be
available at their booth at the Technology from Russia '94 exposition
in the Washington Convention Center, May 10-12 at booth 117. Admission
to the exhibit area is $10.00.  If you are unable to attend the
exposition, but would like to order copies of the guides, you may do
so by phone, fax, email or mail. Send request for order information
to:  SSI/SBA, P.O. Box 82, Princeton, NJ 08542; 609-921-3543; fax:
609-921-0389; or email: <p01375@psilink.com>.  The guides are not
available in electronic format. 

% ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ======
% Date: Fri, 29 Apr 94 16:18:11 EDT
% Errors-To: mjames@lfkw2.bgm.link.com
% Reply-To: ssi_mail@espsun.bgm.link.com
% Originator: ssi_mail@espsun.bgm.link.com
% Sender: ssi_mail@espsun.bgm.link.com
% From: "Space Studies Institute" <p01375@psilink.com>
% Subject: NPO Energia: MIR Handbook
% X-Listserver-Version: 6.0 -- UNIX ListServer by Anastasios Kotsikonas
% X-Comment: SSI Members email Discussion Group

225.36ASCII diagram and radio frequenciesMTWAIN::KLAESKeep Looking UpSun May 29 1994 17:57127
From:	US4RMC::"magliaco@pilot.njin.net" "John Magliacane" 28-MAY-1994 
To:	usenet-space-news@arc.nasa.gov
CC:	
Subj:	* SpaceNews 31-May-94 *

SB NEWS @ AMSAT $SPC0531
* SpaceNews 31-May-94 *
 
BID: $SPC0531
 
                               =========
                               SpaceNews
                               =========
 
                           MONDAY MAY 31, 1994
 
SpaceNews originates at KD2BD in Wall Township, New Jersey, USA.  It is
published every week and is made available for unlimited distribution.
 
* MIR DIAGRAM * 
===============
The following graphic depicting the structure of the Mir space station is
provided by Jean-Claude, FB1RCI:
 
MIR complex: ex-CCCP/Russian space station (Launch 1986) 90 tons
 
                                        _   EVA hatchway
                                      /   \
    attitude motor                  /       \
       control                     I         I
           O                       I         I   KRISTAL
            \                      I         I   module
             \                     I         I
              \      docking   n   I_       _I
               \                 o   \     /
    _____     __\______           d   I   I
   I      \_/           \________   e  \_/     _    _____/I
   I                              \__ /   \  /   \/       I  SOYOUZ
   I                               __   +  I              I  shuttle
   I       _             _______ /    \ _ /  \ _ / \_____ I
   I ___ /   \_________ /             /    \             \I
                                     I      I
   KVANT 1     Domestic/Command     I        I
   module            area           I        I
                 (main module)      I        I  KVANT 2
                                    I        I  module
                                    I        I
                                     \__   __/
                                         \/ docking gear
      I\_____    _
      I       \/   \   automatic freighter
      I             I       PROGRESS
      I _____ /\ _ /
      I/
 
Professional frequencies:

   FM      143.625  MHz  downlink to the ground control station TSUP (voice)
   FM      121.750  MHz     --     for Mir extra vehicular activity (voice)
   FM      121.750  MHz     --     for Soyuz approach for docking (voice)
  SSB      922.750  MHz     --     for telemetric Mir (few moments)
  SSB      166.150  MHz     --     for telemetric Progress freighter

Radio amateur frequency:

  FM       145.550  MHz     up/downlink  voice contact (CQ MIR)
 FM+AFSK   145.550  MHz     --    --     AX.25 packet PMS 1200 bps (R0MIR-1)
 

* REPORT FROM DL3HRT *
======================
Karsten Hansky, DL3HRT, reports that he is active on RS-10 and monitors
the satellite especially during passes in range of North America, but hears
few signals.  He has worked VE2AYT and K1QPM so far.  Both stations come in 
with good signals (559).  Karsten has also worked CN8ST and has heard a 
TU4-station on the satellite.
 
DL3HRT recently made a test and heard his own downlink signals using an 
uplink power of just 300 milliwatts fed into a 9-element yagi.  He feels 
this success should encourage others to try RS-10 Mode A operations.
 
In other news, Karsten, along with Matthias, DL3HZM, have created a 
satellite tracking program called "sat09may.exe" that is available via 
anonymous FTP at igel.physik.th-zwickau.de in the /pub subdirectory, and
pilot.njin.net in the /pub/SpaceNews/software subdirectory.  An older
version is available from the Simtel directory at oak.oakland.edu.
 
* THANKS! *
===========
Thanks to all those who sent messages of appreciation to SpaceNews, especially:
 
        KA3AFY   KB4ZTN   WD5EEV   KH6AF   K7YHA   N8QPO   NX0R
        Harry Bedard, Jr. Don Fay
 
* FEEDBACK/INPUT WELCOMED *
===========================
Mail to SpaceNews should be directed to the editor (John, KD2BD) via any
of the following paths:
 
FAX      : 1-908-747-7107
PACKET   : KD2BD @ N2KZH.NJ.USA.NA
INTERNET : kd2bd@ka2qhd.de.com -or- kd2bd@amsat.org
 
MAIL     : John A. Magliacane, KD2BD
           Department of Engineering and Technology
           Advanced Technology Center
           Brookdale Community College
           Lincroft, New Jersey  07738
           U.S.A.
 
       <<=- SpaceNews: The first amateur newsletter read in space! -=>> 
 
--
John A. Magliacane, KD2BD   * /\/\ * Voice   : 1-908-224-2948
Advanced Technology Center  |/\/\/\| Packet  : KD2BD @ N2KZH.NJ.USA.NA
Brookdale Community College |\/\/\/| Internet: kd2bd@ka2qhd.de.com
Lincroft, NJ  07738         * \/\/ * Morse   : -.-  -..  ..---  -...  -..

% ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ======
% Subject: * SpaceNews 31-May-94 *
% Followup-To: rec.radio.amateur.space,sci.space
% Approved: rec-radio-info@ve6mgs.ampr.ab.ca
% Date: Fri, 27 May 1994 13:17:59 MDT
% From: magliaco@pilot.njin.net (John Magliacane)
% Newsgroups: rec.radio.amateur.space,sci.space.news,rec.radio.info
% Apparently-To: usenet-space-news@arc.nasa.gov

225.37Radio frequenciesMTWAIN::KLAESKeep Looking UpTue Jun 07 1994 14:2265
From:	US4RMC::"magliaco@pilot.njin.net" "John Magliacane"  7-JUN-1994 
To:	usenet-space-news@arc.nasa.gov
CC:	
Subj:	* SpaceNews 06-Jun-94 *

SB NEWS @ AMSAT $SPC0606
* SpaceNews 06-Jun-94 *
 
BID: $SPC0606
 
                               =========
                               SpaceNews
                               =========
 
                           MONDAY JUNE 6, 1994
 
SpaceNews originates at KD2BD in Wall Township, New Jersey, USA.  It is
published every week and is made available for unlimited distribution.
 
* MIR INFORMATION *
===================
Sven Grahn of Sollentuna, Sweden provided the following information 
regarding the frequencies and emissions used by the Mir space station.
 
Sven reports the signals on 166 MHz are PCM FM signals and the modulation 
index is so high that two peaks appear in the signal spectrum, one on 
each side of the carrier.  The carrier is on 166.000 MHz creating a signal 
peak at 166.150 MHz and another peak at 165.850 MHz.
 
The signals from Soyuz and Progress on 922.75 MHz contain a carrier plus 
telemetry sidebands.  The modulation type is unknown.  Sometimes tones 
are frequency modulated on the carrier.  These contain sixteen-bit words, 
which probably constitute a command verification link.  There is a similar 
link from Soyuz and Progress on 926.07 MHz operating simultaneously with 
the 922.75 MHz link.
 
For Progress and Soyuz, the 922, 926 and 166 MHz signals are switched on 
simultaneously by ground command.
 
[Info via Sven Grahn]
 
* FEEDBACK/INPUT WELCOMED *
===========================
Mail to SpaceNews should be directed to the editor (John, KD2BD) via any
of the following paths:
 
FAX      : 1-908-747-7107
PACKET   : KD2BD @ N2KZH.NJ.USA.NA
INTERNET : kd2bd@ka2qhd.de.com -or- kd2bd@amsat.org
 
MAIL     : John A. Magliacane, KD2BD
           Department of Engineering and Technology
           Advanced Technology Center
           Brookdale Community College
           Lincroft, New Jersey  07738
           U.S.A.
 
       <<=- SpaceNews: The first amateur newsletter read in space! -=>> 
 
--
John A. Magliacane, KD2BD   * /\/\ * Voice   : 1-908-224-2948
Advanced Technology Center  |/\/\/\| Packet  : KD2BD @ N2KZH.NJ.USA.NA
Brookdale Community College |\/\/\/| Internet: kd2bd@ka2qhd.de.com
Lincroft, NJ  07738         * \/\/ * Morse   : -.-  -..  ..---  -...  -..

225.38MIR visibile over United KingdomMTWAIN::KLAESKeep Looking UpMon Jun 20 1994 17:1338
Article: 61569
From: ai@iol.ie (Astronomy Ireland)
Newsgroups: sci.astro,sci.space.policy
Subject: Mir visible over UK daily until June 28th
Date: 19 Jun 1994 21:36:51 GMT
Organization: Ireland On-Line
 
The Russian manned space station Mir is visible high over the U.K.
every evening from now (June 19) to Tuesday June 28th. 
 
There are three men on board:- Dr. Valeri Poliakov, Viktor Afanasyev
and Yuri Usachov. All have been on board since January 10. 
 
The craft is very bright. I saw it last night at about magnitude -2 or
-3. Not surprising since it is the largest man-made object in space
and about as low as it can be without burning up. 
 
The time to see it each evening is issued on the 0891-88-1950 each day
for that evening for just a 10p call (remember the last six digits as
eighty-eight nineteen-fifty). Please tell non-computing friends this
number. A file is available on the internet containing less frequently
updated listings (for Ireland - add 1 minute for mainland U.K.) at
ftp.iol.ie in /users/ai/ai-iol.mir (but remember, the very latest
predictions for the U.K. are always on the hotline number below - which, 
by the way, is updated every Monday with the latest news of what to see 
whether Mir is around or not - now running for nearly 2 years). 
 
Reports of sightings welcome. If you feel up to, the time (to the
second) of when Mir passes above or below any naked eye star would be
useful to me. Give your latitude, longitude, height above sea-level,
date and source of time signals used. Thanks. 
 
--
David Moore BSc FRAS, Editor of "Astronomy & Space" magazine.
(ai@iol.ie) Chairman, Astronomy Ireland, P.O.Box 2888, Dublin 1.
Tel: +353-1-459 8883. Fax: +353-1-459 9933. Irish News: 1550-111-442
____________________U. K. NEWSLINE: 0891-88-1950____________________

225.39MIR visible over North America all night longMTWAIN::KLAESKeep Looking UpTue Jun 21 1994 12:4835
From:	US4RMC::"ASTRO%GITVM1.BITNET@uga.cc.uga.edu" "Astronomy Discussion 
        List" 21-JUN-1994 07:36:39.57
To:	Multiple recipients of list ASTRO <ASTRO%GITVM1.BITNET@uga.cc.uga.edu>
CC:	
Subj:	MIR, RUSSIAN SPACE STATION

I don't know if anyone will consider this of interest to an *ASTRO*
discussion group, but for the next several days the orbital track of
the Russian space station, MIR, is lined up very close to the
terminator; this results in the satellite remaining in sunlight for
several days, without dipping into the Earth's shadow.  Therefore the
satellite is visible on every pass all night long (from North America); 
it is illuminated over the polar regions during the wee hours. 

Look tonight at 2200 MDT, and approx every 90 minutes after; it will
rise in the Southwest and track toward the Northeast at 2200, but each
pass is different (obviously).  All passes are basically from West to
East, tho'. 

I'm still interested in comments on the INTES 6 inch Mak.

Clear Skies...

Norm   <normhansen@delphi.com>
Mountain Green, Utah

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% Date:         Fri, 17 Jun 1994 20:03:19 -0400
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% From: Norm Hansen <NORMHANSEN@DELPHI.COM>
% Subject:      MIR, RUSSIAN SPACE STATION
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225.40MIR & SOYUZ-T18 docking or exchanging crews?4371::BATTERSBYTue Jun 21 1994 16:1520
225.41Mistake?skylab.zko.dec.com::FISHERCarp Diem : Fish the DayTue Jun 21 1994 16:3016
Notice that Soyuz TM-18 is object 94001A, implying that it was the first object
launched in 1994.  Presumably, that means it was launched in January some time.
That implies to me that either

1)  It is attached to MIR, but they did not update the elements

2)  It is drifting around

3)  It reentered normally but was mistakenly not taken of the list.


I'd bet on 1 or 3.  

Just guessing,

Burns
225.42MIR Orbit AdjustmentsMTWAIN::KLAESHouston, Tranquility Base here...Wed Jul 20 1994 16:4475
From:	US4RMC::"magliaco@pilot.njin.net" "John Magliacane" 19-JUL-1994 
To:	usenet-space-news@arc.nasa.gov
CC:	
Subj:	* SpaceNews 18-Jul-94 *

SB NEWS @ AMSAT $SPC0718
* SpaceNews 18-Jul-94 *
 
BID: $SPC0718

                               =========
                               SpaceNews
                               =========
 
                          MONDAY JULY 18, 1994
 
SpaceNews originates at KD2BD in Wall Township, New Jersey, USA.  It is
published every week and is made available for unlimited distribution.
 
* MIR ORBIT ADJUSTMENTS *
=========================
The following graphic depicts the mean motion (which is inversely 
proportional to mean orbital altitude) of Mir over the past several months:
 
          TIME REVOLUTION (summary)  for  MIR Complex 16609
                (Period= day 130 to day 185 1994)
 
       revolution/day
          I
 15.5500  I
          I
 15.5600  I      ______
          I     I       \_______
 15.5700  I     I                \_____
          I     I
 15.5800  I     I
          I_____I
          I
 15.6000  I
          I
          I
 15.6500  I                                                       Epoch time
          Ix___________x____________x___________x___________x___________x__
           May         Jun         Jul         Sep         Oct         Nov
 
 
Orbit adjustments were made on 12-March, 12-May, and on 03-July when Mir 
docked with the Soyuz TM-19 module.
 
[Info via Jean-Claude, FB1RCI]    
 
 FEEDBACK/INPUT WELCOMED *
===========================
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any of the following paths: 
 
FAX      : 1-908-747-7107
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MAIL     : John A. Magliacane, KD2BD
           Department of Engineering and Technology
           Advanced Technology Center
           Brookdale Community College
           Lincroft, New Jersey  07738
           U.S.A.
 
       <<=- SpaceNews: The first amateur newsletter read in space! -=>> 
 
--
John A. Magliacane, KD2BD   * /\/\ * Voice   : 1-908-224-2948
Advanced Technology Center  |/\/\/\| Packet  : KD2BD @ N2KZH.NJ.USA.NA
Brookdale Community College |\/\/\/| Internet: magliaco@pilot.njin.net
Lincroft, NJ  07738         * \/\/ * Morse   : -.-  -..  ..---  -...  -..

225.43Extracted from Jonathans Space report #215 MIR config etc.56821::BATTERSBYThu Oct 20 1994 15:5717
    
    Jonathan's Space Report
    No. 215               1994 Oct  18               Cambridge, MA
    --------------------------------------------------------------------------------
    
    Mir
    ---
    
    The Mir complex is undergoing power difficulties and the crew's
    experiments were interrupted for several days. The station's
    solar panels will be in a more favorable orientation this
    week and normal operations should resume. The Mir complex
    consists of the core module, the Kvant astrophysical module,
    the Kvant-2 airlock module, and the Kristall module. Soyuz TM-19
    is docked at the Kvant rear port and Soyuz TM-20 is docked at
    the Mir forward port.