Saturday, June 27, 1992

STS-4 (Columbia)

 1982-065A


STS-4 was the fourth and last Orbital Test Flight mission. Launch of STS-4 was at 1500:00 on 1982 Jun 27. After four OMS burns, Columbia entered a 295 x 303 km x 28.5 deg orbit. The crew ran into a major payload problem when the aperture door on the CIRRIS telescope failed to deploy. On Jun 29, it was time for more tests of the RMS. The RMS grappled the Induced Environment Contamination Monitor and moved it around the bay to make contamination measurements. The next two days saw more tests of the payload bay doors and of the RCS and OMS engines. At 1100 on Jul 2, Mattingly tested out the new EVA spacesuit. Later that day, more RCS burns were used to test the dynamics of the RMS arm. Columbia landed at Edwards AFB on Jul 4.


STS-4 
 

DateTimeEventOrbit  

1982 May 18   Rollover  VAB/3 
1982 May 25   ET mate 
1982 May 26   Rollout  LC39A 
1982 Jun 27  1500:00  Launch, LC39A 
 1502:10  SRB sep (47.6 km) 
 1508:33  MECO 
 1508:50  ET sep (108.1 km)  86.04 -17 x 172 x 28.5 
   86.03 -13 x 168 x 28.5 
 1510:33  OMS-1 (88s) 46.6m/s 87.58 63 x 241 x 28.5 
 1512:01  OMS-1 CO 
 1526ET apogee 
 1537:41  OMS-2 (104s) 53.1m/s   
 1539:26  OMS-2 CO  
 1547  ET breakup 
 1701  PLBD open  89.38 237 x 249 x 28.5 
 1929:13  OMS 3 (32s) 16m/s  89.98 249 x 296 x 28.5 
 2014:11  OMS 4 (32s) 16m/s 90.54 296 x 304 x 28.52 
1982 Jun 29   RMS grapple IECM 
 1217  RMS unberth IECM 
 1532  RMS reberth IECM 
 1600  RMS unberth IECM  90.52 296 x 303 x 28.5 
 1812  RMS reberth IECM 
 1950RCS burn
1982 Jun 30  0553   90.56 297 x 306 x 28.5 
1982 Jun 30  1748  PLBD closed  
 1956  PLBD open 
1982 Jul 1  1026  PLBD closed 
 1113  PLBD open 
 1330  RCS  90.55 296 x 306 x 28.5 
 1345  RCS  
 1833  OMS 5 (LH, 17s) 4.5m/s 90.70 304 x 312 x 28.5 
1982 Jul 2  0855  RCS   
 1055  RCS  90.73 301 x 319 x 28.5 
 1659  RCS (RMS test)   
 1741  RCS (RMS test)   
  RCS  89.77 302 x 322 x 28.5 
1982 Jul 4  0152   90.77 300 x 324 x 28.5 
1982 Jul 4  1147  Begin to close PLBD  90.77 305 x 318 x 28.5 
 1211  PLBD closed   
 1510:00  OMS DO (171s) 94.2m/s 
 1512:53  OMS DO CO 
 1540:23  Entry 
 1609:40  Landing  RW22 EAFB 
 1609:53  NGTD 
 1610:54  Wheels stop 
1982 Jul 14  1446  SCA  Dyess AFB, TX 
1982 Jul 15  1430  SCA arr. KSC  KSC SLF 
1982 Jul 16  0100OPF/1 

Payload:

  • R-11 (DoD 82-1)

  • DFI Development Flight Instrumentation

  • IECM Induced Environment Contamination Monitor

  • ACIP

  • G-001 GAS (Utah State University/R. Gilbert Moore) Fruit flies, brine shrimp, duckweed, algae, Composite curing,soldering, alloy formation, Surface tension, thermal conductivity, System thermal survey. (Power and electrical problems)

  • Middeck

  • MLR Monodisperse Latex Reactor

  • CFES1 Continuous Flow Electrophoresis System 

Friday, June 26, 1992

Kosmos 803

  1976-014A


This target satellite was intercepted by Kosmos 804.


Kosmos-803 
 

DateTimeEventOrbit  

1976 Feb 12  1300 Launch by 11K65M  PL 
 1308  Stage 2 MECO-1 
 1330?  Stage 2 MECO-2
1976 Feb 15  96.4 554x618x65.9 

Thursday, June 25, 1992

Gemini 10

  1966-066A


Gemini 10 was crewed by John Young and Michael Collins. The mission saw rendezvous with both TDA 5 and TDA 3, the Gemini 8 target vehicle.

In the 25-minute EVA, Collins used the gas gun to propel himself across open space to the Agena. In the course of two trips he retrieved a micrometeorite package from TDA 3. The cabin was repressurized after 40 min 8 s. It was depressurized a final time at 0052 on Jul 21 for a 2 min 52s equipment dump.

Retrofire was 92.8m/s aft, 35.4 m/s down, 20 deg pitch down. The spacecraft was recovered from the Atlantic by the USS Guadalcanal after a splashdown at 26 44 07 N 71 57 W.


GTA-10 mission events 
 

DateTimeEventOrbit  

 
1966 Jul 18  2220:27  Launch 
 2222:59  BECO, staging T+2:32  -5941 x 120 x 29.4  
 2226:07  T+5:40 SECO  160 x 166 x 29.0  
 2226  Orbit insertion 
 2226:38 T+6:11 Stage 2 sep  160 x 259 x 29.0 
 2227:13  IVAR 7.6m/s  160 x 268  
 2227:48  T+7:21 OAMS off 
 2231  Pilot window cover ejected 

1966 Jul 19  

0038:36  NC1 phase adjust 17m/s 1:16  217 x 268 x 29.01 
 0050:49  NPC plane change 2.9m/s 0:13  
 0056   88.73 162 x 261 x 28.9 (TLE) 
 0208:03  NSR coelliptic circ 15m/s 1:05 
 0254:11  TPI 10m/s
 0306:50  CORR-1 VY = 6.2m/s 
 0318:51  CORR-2 VX = 8.8m/s 
 0320  Range 2 km 
 0322:19  TPF 15m/s
 0332  At 180m holding 
 0342  Rendezvous with GATV 5005 at 12m 
 0413:03  Docked with TDA 
 0558:44  SPS burn 1:38 
 0559:00  NCH1 phase adj (docked PPS, 13s) 128m/s 294 x 763  
 0600?   95.21 299 x 757 x 28.8 (TLE) 
 0700?  S-12 collector opened 
 1840:24  NH SPS burn 1:35 T+20:20 
 1840:38  NCH2 height adjust (docked PPS, 11s) 102 m/s  297 x 386  
 2057  NSR SPS 1:28 
 2057:32  T+22:38 NSR circ burn, 26m/s docked PPS 4s  378 x 386  
 2106:02  Phasing, SPS 10s  379 x 389  
 2140  At 4psi 
 2143:52  Depress T+23:24  
 2144:30? Hatch open, SEVA UV photos 
 2145  Waste Bag jettisoned (1kg?) 
 2150  Begin S-13 UV photos 
 2229?  MSC-8 plate and rod jettisoned 
 2230  Collins problems with eye irritation 
 2232:35  S-13 bracket jettison 
 2233  Hatch closed 
 2234:12  Repress 
1966 Jul 20  0206:02s NC1 catch-up, SPS thrusters, 0:09 3m/s T+27:45:35 
1966 Jul 20  1524:52  Plane change 5m/s, SPS 18s  380 x 388  
 1556:16  Phase adjust 1m/s ret SPS 4s  380 x 380 
 1642  Suit test, depress to 3psi 
 1740  End ECS test, repress 
 1900:03  Undocked from TDA/Agena 5005 0.5m/s 3s 
  Range to Agena 5003 250km 
  Sep to 6m, begin S-26 Ion Wake during sep 
 1914  Jettison CDR window cover 
 1916  At 450m from GATV5005 
  Begin Agena rendezvous 
 2014:28  NCC corrective burn T+45:54:01 1m/s  
 2029:55  NSR coelliptic T+46:09:28 3m/s  385 x 385? 
 2147:11  TPI 30s 9m/s  
 2154:37  CORR-1 
 2159:25  CORR-2 
 2159:37  TPF 5 km 
 2203  R-dot 15m/s 
 2212  At 200m 
 2217  Stationkeeping 
 2217  Rendezvous with TDA/Agena 5003  398 x 398? 
 2241  At 2m 
 2256  Begin depress 
 2301:14  Depress  
 2301  Hatch open, PLT egress; 6m range to Agena 
 2307  Retr S-12 experiment from GT exterior  
  S-12 nose fairing discarded 
 2310?  PLT transfer to AM 
  Plug in N2 line for HHMU 
  2m to Agena 
 2316  PLT transfer to TDA 
 2317  PLT leaves Agena 
 2317  PLT 6m from Gemini 
 2318  PLT Back at cabin 
 2319  PLT leave Gemini to Agena (5m) 
 2320  PLT at TDA 
 2323  Retrieve S-10 from Agena 
 2323?  Accidental release of Hasselblad 
 2323  PLT leave Agena 
 2324  PLT at cabin 
 2326  Jettison new S-10 
 2326?  Flight plan floats out of hatch
 2326?  S-12 experiment floats out 
 2340  Hatch closed 
 2341:22  Repress  
1966 Jul 21  0052:22  Depress 
 0053  Hatch open,equipment dump 
  Jettison ELSS chest pack 
  Jettison Umbilical Bag with 15m umbilical, 
  HHMU, 
  Standup hoses (0.6m) 
  Y connectors (x2), Suit hose interconnect 
  EVA visor; EVA light; dry waste container (x2) 
  Glare shield; S-12 fairing 
 0054  Hatch closed 
 0055:14  Repress 
 0136:27  Lateral sep, 0.3m/s 
 0159:18  Orbit shape burn, lower peri 30m/s 1:57  292 x 400 
 2029:01  AM sep  300 x 398 x 28.9 (SR4) 
 2030:53  Retrofire 
 2031:46  RM sep and docking bar sep -10 x 392 x 28.9  
 2053:18  117 km  -4 x 406 x 29.0 (SR4) 
 2107:05  Splashdown 
 2134  Recovered by USS Guadalcanal 

GATV-5

  1966-065A


TDA 1A was launched aboard Gemini Agena Target Vehicle 5005, to serve as the target for Gemini 10. After the Gemini 10 encounter, the primary engine was used to raise the orbit and then lower it again, carrying out temperature tests on the payload. A third burn by the secondary propulsion system placed it in a storage orbit for use as a reserve target.


TDA 1A 
 

DateTimeEventOrbit  

1966 Jul 18  2039:46  Launch from LC14 
 2041:56  T+2:10 BECO  -5948 x 132 x 28.9  
 2041:58  T+2:13 Booster sep 
 2044:24  T+4:39 SECO 
 2044:44  T+4:58 VECO 217 km  -4404 x 292 x 29.0 
 2044:46 T+5:00 Atlas sep 
 2045:37 T+5:51 Agena SPS ignition 
 2045:56  T+6:10 Agena PPS burn 
 2046:16  T+6:20 Fairing 
 2049:06  T+9:20 Agena MECO 
 2049  Orbit insertion 
 2105TDA activated 
 2324   90.42 292 x 298 x 28.9 
1996 Jul 19  0413:03  Gemini 10 docked with TDA 
 0559:00  Phase adj (docked PPS, 13s)  294 x 763  
 0600?   95.21 299 x 757 x 28.8 (TLE) 
 1840:38  Height adjust (docked PPS, 10s)  297 x 386  
 2057:32  Circ burn, docked PPS 2s  378 x 386  
 2106:02  Phasing, SPS 10s  379 x 389  
1966 Jul 20  1524:52  Plane change, SPS 18s  380 x 388  
 1556:16  Phasing burn 4s  380 x 380 
 1900:03  Gemini 10 undocked 
1966 Jul 21  2241:32  PPS burn 257m/s 385 x 1390  
1966 Jul 22  0508:05  PPS burn 264m/s 352 x 383  
1966 Jul 22  0918:33  SPS burn 10m/s 352 x 347  
1966 Jul 23  1906   91.52 347 x 351 x 28.9 
1966 Jul 25  1200?  End of transmissions 
1966 Jul 26  2010   91.51 345 x 351 x 28.9 
1966 Jul 31    91.48 344 x 350 x 28.9 
1966 Aug 20  91.42 340 x 348 x 28.9 
1966 Nov 14    90.50 297 x 300 x 28.9 
1966 Dec 25   88.75 209 x 215 x 28.9 
1966 Dec 29   Reentered 

Star Tracks

https://welib.org/md5/03790b7513044798f60986331dcac69a

Teen: February 1992

 https://welib.org/md5/df37563e509cded8cf5f803273ac3945

Club Management: November 1991

 https://welib.org/md5/96406372946c308b9de62653a670ec35

Spaceflight: January 1992

 https://welib.org/md5/45483459db23d4bedd5d7fc2d8fa273d

Aviation Week: February 3,1992

 https://welib.org/md5/6731efe15a39e5fa6182013bd47def02

Monday, June 22, 1992

ASTEX

 1971-089A


The P71-2 satellite, also known as ASTEX (Advanced Space Technology Experiments), was launched on 1971 Oct 17 by a Long Tank Thrust Augmented Thor Agena D from Vandenberg. The spacecraft used an Agena D satellite bus.

CMP/SAMSO-002 was an IR astronomy experiment. According to Price the sensor was forced to scan along the horizon rather than at the zenith because of other payload requirements, and a cryocooler line leak ended the experiment after two weeks. CMP returned only three orbits of data but covered 82 percent of the sky in two bands.

The FRUSA (RTD-806) array was used in the design of the HST solar arrays. The ONR-001 experiment was to understand what happens to the ionosphere during a high altitude nuclear explosion; it seems to have used a solar storm to model this. NSA-001 was an experimental secure communications link. Known payloads had a mass of 217 kg.


P71-2 
 

DateTimeEventOrbit  

1971 Oct 17  1336 Launch by Thorad Agena D  
 1338  VECO 
 1338  Thor sep 
 1338  Agena D burn 
 1343?  Agena D MECO 
 1430? MES-2 
 1431? MECO-2 
   100.7 773 x 803 x 92.7 
1973 Dec   Still operating 

Payload:

  • CMP Celestial IR Mapping Program (SAMSO-002), 58 kg, studied IR background

  • FRUSA Flexible Rolled Up Solar Array 9.75m (RTD-806), 113 kg

  • NSA-001 NSA command and control interfaces, 8 kg

  • ONR-001, LPARL payload, Study solar storm effects on polar phenomena, for modelling nuclear detonation effects on ionosphere, 38 kg

    • ERIS Earth Reflecting Ionospheric Sounder (LPARL/)

    • High resolution electron spectrometers (LPARL/Imhof) 

    • HEAPS High energy alpha-proton spectroemters (LPARL/Reagan) 

    • HEPS High Energy Proton Spectrometer (LPARL/Reagan)

Progress 35

 1988-024A


Progress No. 143 (7K-TG No. 143) was launched in Mar 1988. It was announced as Progress-35. It carried 2283 kg of cargo.


Progress-35 
 

DateTimeEventOrbit  

1988 Mar 23  2105:12  Launch by Soyuz-U  KB 
 2114  Blok-I sep 
 2200   88.97 185 x 262 x 51.6 
1988 Mar 24  0700   88.80 183 x 248 x 51.6 
 2200   88.76 182 x 245 x 51.6 
1988 Mar 25  0500   89.75 240 x 285 x 51.6 
 2221:35  Docked with Mir, Kvant DP2 
 2316   91.20 308 x 359 x 51.6 
1988 Mar 26  1700   91.18 318 x 347 x 51.6 
1988 May 5  0136:03 Undocked 
 0430?88-24C separated 
 0612?  Deorbited 
 0656:19  Reentered 

May 13,2026

  https://planet4589.org/space/jsr/back/news.855.txt