Saturday, December 6, 1997

Kosmos 185

  1967-104A


The first test flight of the 11K67 (Tsiklon-2A) launch vehicle placed a test satellite, I-2BM or IS-104 (GVM) in orbit on 1967 Oct 27. The GVM was named Kosmos-185. It appears to have included a functional DU propulsion system.


Kosmos-185 
 

DateTimeEventOrbit  

1967 Oct 27  0221:19  Launch by 11K67  KB 
 0223  Stage 2 burn  
 0226?  Stage 2 MECO  
 0900 98.67 518 x 871 x 64.1 
1967 Oct 29  1139  (DU orbit) 98.59 509 x 873 x 64.1 
1967 Nov 4  1222  (DU orbit) 98.66 517 x 872 x 64.1 
1968 Nov 15  1003   94.95 425 x 606 x 64.05 
1969 Jan 14  1507   88.79 214 x 214 x 64.0 
1969 Jan 14   Reentered 

Apollo 17 (America)

 1972-096A



    Apollo 17 Crew

  • CDR Commander Eugene Cernan, Capt. USN

  • CMP Command Module Pilot Ronald Evans, Cdr USN

  • LMP Lunar Module Pilot Harrison `Jack' Schmitt, Ph.D., NASA

Apollo CSM 114 was the CSM for the Apollo 17 mission. The crew named it America. Apollo 17 was launched at 0533 on 1972 Dec 7 from Launch Complex 39A at Kennedy Space Center. The Saturn V SA-512 delivered Apollo 17 to a 169 x 178 km Earth orbit at 0544.

The S-IVB reignited for translunar injection at 0845. Half an hour later the CSM separated from the Spacecraft Lunar Adapter, the four SLA panels ejected into space. The crew rotated the CSM and came back in to dock with the exposed Lunar Module. The transposition and docking maneuver was complete at 0929, and at 1018 the assembled Apollo 17 spaceship separated from the S-IVB stage.

The crew made a single midcourse correction on the way to the Moon, and a few hours before arrival jettisoned the panel covering the instruments in the SIM (Scientific Instrument Module). The SIM carried the Lunar Sounder, a synthetic aperture radar system operating at 5, 15 and 150 MHz.

Apollo 17 entered lunar orbit with a firing of the CSM's SPS engine at 1947 on Dec 10. On Dec 11, Cernan and Schmitt transferred to the LM, leaving Ron Evans as the sole crewmember aboard America.

At 1721 on Dec 11 the LM Challenger undocked and began its descent to the Moon. Evans changed America's orbit to 100 x 130 km and concentrated on lunar orbit science operations. Two more orbit changes were made on Dec 14, and early on Dec 15 Challenger, back in space, approached the CSM. Challenger docked with America at 0110:15 and Cernan and Schmitt returned to the CM with their cargo of lunar rock. The LM was undocked at 0451 on Dec 15.

The voyage home began at 2335 on Dec 16 with the transearth injection burn. At 2027:40 on Dec 17 the cabin was depressurized. The CMP exited the hatch and translated along the Service Module to the SIM bay, retrieving the panoramic, mapping, and lunar sounder film and data cassettes in three trips. The LMP stood in the hatch and assisted. The hatch was open for 45 minutes, and the CM was depressurized for 1:05:44, until 2133:24. (Another source gives 1:07:18).

On Dec 19 the Service Module was jettisoned and the Command Module began its reentry, with the nominal start of reentry at 1911:38. America splashed down in the Pacific at 1925, and was recovered by the USS Ticonderoga.



CSM 114 Mission Log 
 

DateTimeEventOrbit  

1972 Dec 7  0533:00 Launch 
1972 Dec 7  0535:19 S-IC center engine cutoff 
1972 Dec 7  0535:41 Outboard engine cutoff 
1972 Dec 7  0535:43 S-IC stage separation, S-II ignition 
1972 Dec 7  0535:45 Interstage separation 
1972 Dec 7  0536:19 LES separation 
1972 Dec 7  0540:41 S-II center engine cutoff 
1972 Dec 7  0542:19 S-II outboard engine cutoff 
1972 Dec 7  0542:19 S-II stage separation 
1972 Dec 7  0542:21 S-IVB-512 ignition 
1972 Dec 7  0544:42 S-IVB-512 main engine cutoff 
1972 Dec 7  0544:52 Orbit insertion  167 x 172  
 0556  Optics cover off 
1972 Dec 7  0845:37 S-IVB-512 reignites for a 5m51s TLI burn 3.157km/s  
  139842 kg at TIG, 180 km alt 
1972 Dec 7  0851:38 Translunar injection (TLI) at 280 km 10.846km/s 
1972 Dec 7 0915:29 CSM separates from S-IVB/SLA 
1972 Dec 7 0929:45 CSM 114 docks with LM 12 (attached to S-IVB) 
 0930  Hard dock, partial latch problem 
1972 Dec 7 1018:00 CSM 114/LM 12 separate from S-IVB-512 
  Mass 30317 kg; CSM on impact trajectory prior to MCC2 
  LM mass 16456 kg 
 2233  CSM pass EL4:1 
 2340  S-IVB pass EL4:1 
1972 Dec 8 1703:00 MCC-2 midcourse correction 2s 3m/s, periline 96 km  
1972 Dec 10 0410:45 Equigravisphere 
1972 Dec 10 1505:40 SIMbay panel jettison 382000 km range 
1972 Dec 10 1947:23 LOI-1 lunar orbit insertion burn (SPS)  
  910 m/s 6:38 
1972 Dec 10 1953:56 Lunar orbit insertion  97 x 315 km 
1972 Dec 11 0004:37 LOI-2/DOI burn 60m/s 22s 26 x 109 km 
 1430  23 x 111 
1972 Dec 11 1440? CDR and LMP transfer to LM 12. 
 1600? HC to LM 
1972 Dec 11 1720:56 LM 12 undocking 
1972 Dec 11 1721 RCS separation burn 
1972 Dec 11 1850:29 Circularization burn, 100 x 130 km orbit 
1972 Dec 14 1627:05 Trim burn to 115 x 124 km 
1972 Dec 14 1726:54 LOPC-1 lunar orbit plane change burn, to 116 x 116 km 
1972 Dec 15 0110:15 LM 12 docked with CSM 114 
1972 Dec 15 CDR and LMP return to CSM 114
1972 Dec 15 0451:31 LM 12 undocked 
  CSM mass 16576 kg 
1972 Dec 15 0456:31 Separation burn, to 113 x 118 km 
1972 Dec 16 2335:09 SPS Transearth Injection (TEI) burn 
1972 Dec 16 2337:33 CSM 114 leaves lunar orbit 
1972 Dec 17 1332? Leave lunar sphere 
1972 Dec 17 2027:40 EVA depress 
 2031  HO 
 2032? Jett bag? 
 2037  CMP egress 
 2119  CMP ingress 
 2120  HC 
 2123  Begin repress 
 2123  Rep. 0.7psi 
 2134  Rep. 3.5psi 
1972 Dec 19 1611:01 MCC-7 midcourse correction 
1972 Dec 19 1856:49 SM-114 separation 
1972 Dec 19 1911:38 Entry interface 
1972 Dec 19 1924:59 Splashdown in Pacific Ocean 
1972 Dec 19 2128 Recovered by USS Ticonderoga 

Friday, December 5, 1997

Progress M-7

 1991-020A


Progress vehicle 208 (Progress M-7) carried 2542 kg of cargo and the second VBK return capsule. For the first time in the Progress and Progress M program, it failed to dock on the first attempt on 1991 Mar 22. A second approach to Kvant DP2 on Mar 23 also failed, narrowly avoiding a collision. A third attempt using instead the port on the Mir transfer compartment was successful on Mar 28.


Progress M-7 
 

DateTimeEventOrbit  

1991 Mar 19  1305:15  Launch by Soyuz-U  KB 
   88.49 186 x 213 x 51.6 
 2130   89.65 235 x 278 x 51.6 
1991 Mar 21    89.60 237 x 271 x 51.6 
 1700   92.00 358 x 386 x 51.6 
1991 Mar 22  1428  Rendezvous with Mir 100 m 
 1445Failed to dock with Kvant DP2 at 100m 
 1446Flyby Mir at 500m 
 1900   92.14 371 x 387 x 51.6 
1991 Mar 23  1428? Rendezvous 2 with Mir KDP2 
 1442Missed by 5 m 
 1900   92.05 366 x 385 x 51.6 
1991 Mar 25  1200   92.03 364 x 383 x 51.6 
1991 Mar 26  1900   92.02 363 x 382 x 51.6 
1991 Mar 27  1200   92.10 365 x 388 x 51.6 
 1700   92.10 365 x 389 x 51.6 
1991 Mar 28  0500   92.09 365 x 388 x 51.6 
 1202:28  Docked with Mir DP1 
1991 Mar 29  0000   92.02 363 x 384 x 51.6 
1991 May 6  2259:36 Undocked 
1991 May 7  1624  Deorbited 
 1720:05  VBK landing

The face of Venus : the Magellan radar-mapping mission

 https://welib.org/md5/03a0ed1aec93b20fb54ffaf3adb70eba

The World Almanac of the USA

 https://welib.org/md5/335c8b88d31b8e40f89a485dbf2b1edf

Teen: July 1997

 https://welib.org/md5/b15fcde24a05d038e5264a5602211127

Tuesday, December 2, 1997

Kosmos 926

 1977-062A



Kosmos-926 
 

DateTimeEventOrbit  

1977 Jul 8  1730 Launch by 11K65M  Plesetsk 
  T+2:10 St 1 MECO 
  T+2:12 St 1 sep 
  T+2:12 St 2 burn 59km 
  T+2:27 Fairing 76km 
 1738?  T+8:03 St 2 MECO 150 km  150 x 1003? x 83 
  T+1:02:19 St 2 MES2 
  T+1:02:30 St 2 MECO2 
 1833?  T+1:02:50 St 2 sep 
1977 Jul 25   105.1 976x1022x82.9

Journal of the British Interplanetary Society: June 1997

 https://welib.org/md5/ae9176d2f0e291c2b9a18d8d66076782

Friday, November 28, 1997

Journal of the British Interplanetary Society: May 1997

 https://welib.org/md5/af6c054aa58123c54b8e0cafcb32b33d

Spaceflight: May 1997

 https://welib.org/md5/e831e8c41685c54e0121118559e61ae4

The Science fiction reference book : a comprehensive handbook and guide to the history, literature, scholarship, and related activities of the science fiction and fantasy fields

 https://welib.org/md5/4391549efe7904e7d44cf9fdd3af06bd

STS-44 (Atlantis)

 1991-080A


Atlantis deployed the DSP satellite and carried out military experiments. The Terra Scout payload specialist used SPADVOS to study 27 ground targets and carried out the M88-1 experiments to study 16 other ground sites.

The payload bay contained a Protective Cover Removal System (PCRS) which seems to have been related to the DSP payload; presumably some sensor covers on DSP were designed to open before deployment, and perhaps a contingency spacewalk would have been made to remove the covers using tools stored in the PCRS - but this is just speculation.

The mission was cut by 3 days when an IMU malfunctioned on Nov 30 and a Minimum Duration Flight (MDF) was declared.

Atlantis rolled down the runway, with wheels stop at 2236:27 after a no-braking rollout test.


STS-44 
 

DateTimeEventOrbit  

1991 Oct 18   Tow to VAB 
1991 Oct 24   Rollout  LC39A 
1991 Nov 24  2344:00  Launch from LC39A 
 2346:07  SRB sep 
 2352:30  MECO  88.78 70 x 358 x 28.5 (OMS dV) 
 2352:48  ET sep 
1991 Nov 25  0024:48  OMS-2 (3:04) 87m/s 
 0027:52  OMS-2 CO   
 0118  PLBD open  91.81 358 x 367 x 28.5 
 0602  DSP/IUS deployed 
 0617:46  OMS-3 sep 16s 10m/s 92.14 362 x 396 x 28.5 
1991 Nov 26  0600? ARCS-1 orbit lower 75s 
 0653   91.84 361 x 367 x 28.5 
1991 Nov 28  2210  RCS 7s mv avoid r/b K851 91.83 360 x 367 x 28.5 
1991 Nov 30  1514  IMU-2 failed 
 1625MDF (Min Duration Flight) declared 
1991 Dec 1  1845  PLBD closed  91.84 361 x 368 x 28.5 
 2128:16  OMS DO (3:03) 108m/s 
 2131:19  OMS DO CO 
 2203:23  Entry interface 128 km 
 2234:42  Landing RW05 EAFB 
 2234:51  NGTD 
 2236:27  Wheels stop 
1991 Dec 7  1430SCA takeoff  EAFB 
 1815SCA landing  Sheppard AFB, Wichita Falls, TX 
1991 Dec 8  1200SCA takeoff 
 1535SCA landing  KSC SLF 
 1900Tow to OPF  OPF/2 

Wednesday, November 26, 1997

OAO 3

  1972-065A


OAO C carried the Princeton Experiment Package, an 0.8m telescope for ultraviolet spectroscopy of bright stars. Launch was at 1028 on 1972 Aug 21 by Atlas Centaur from Cape Kennedy. The Centaur AC-22 stage ignited for a single 7.5 minute burn at 1032. At 1040 OAO 3 was inserted into a 99.5 min, 736 x 744 km x 35.0 deg orbit. Centaur AC-22 vented its excess propellant at 1045 to make sure the stage would not share OAO 3's orbit. The sun baffle cover was jettisoned on rev 6. After an 8 day test period, Orbiting Astronomical Observatory 3 was declared operational on Aug 29. The satellite was renamed Copernicus in honor of the 500th anniversary of the famous astronomer Nikolai Kopernik (1473-1543). Copernicus carried out astronomical observations until 1980 Dec 30; after a series of engineering tests, it was switched off on 1981 Feb 15.


OAO 3 
 

DateTimeEventOrbit  

1972 Aug 21  1028:02  Launch by Atlas Centaur  CKAFS LC36B 
  T+2:34 BECO  
  T+2:37? Booster sep 
  T+3:16 Insulation panels sep 
  T+3:47 SECO 
  T+3:50 Atlas sep  -5950? x 300? x 35.0 
 1032  T+4:00 Centaur MES 
  T+4:12 Fairing sep 
 1039:26  T+11:24 Centaur MECO  99.5 736 x 744 x 35.0 
  T+11:34 Solar paddles deployed 
  T+11:50 Balance booms extended 
 1040:16  T+12:14 Centaur sep 
  T+25min Centaur blowdown 
 1920  Rev 6 near VAFB 
 1928Sun baffle sep, rev 6 
1972 Aug 29   Operational 
1980 Dec 30   End of ops 
1981 Feb 15   Decommissioned 

Spaceflight: February 1997

 https://welib.org/md5/b43ec7c6350d2a3e363dca883f991e53

Okean 1

 1988-056A


The fifth NKhM spacecraft, Okean-O1 No. 3 (NKhM No. 5) was the first to be given the official post-launch name `Okean'.


Okean-O1 No. 3 
 

DateTimeEventOrbit  

1988 Jul 5  0945:00  Launch by Tsiklon-3  PL LC32/1  
  T+2:00 St 1 sep 
  T+3:33 GO sep 
  T+4:38 St 2 sep 
  T+5:20 S5M burn 1 
 0951  T+6:48 S5M MECO1 
  T+39:20 BOZ burn 
 1025 T+40:58 S5M burn 2  
 1026 T+41:08 S5M MECO2 
  T+41:38 S5M sep 
   97.74 635 x 680 x 82.5 
1995 Jun 14   end of ops 

November 20,2006

  https://en.wikipedia.org/wiki/Association_football