Friday, April 19, 1996

Saturn S-IVB-508

 1970-029B


SA-508 was launched on 1970 Apr 11 at 1913. Apollo 13 separated from the Saturn at 2314, and the S-IVB made its evasive maneuver at 2331 and vented propellants at 2352. At 0112:59 on Apr 12 the stage maneuvered again to set course for lunar impact. S-IVB-508 impacted the lunar surface at 0109:40 on Apr 15 at 2.5S 27.9W. Impact velocity was 2.579 km/s at 15 deg to local vertical.


S-4B-508 
 

DateTimeEventOrbit  

1970 Apr 11  1913:00  Launch by Saturn V (SA-508)  KSC LC39A 
 1915:15  S-IC CECO 
 1915:44  S-IC OECO, S-IC sep 63 km  -6006 x 112 x 31.8  
 1915:46  S-II ignition 
 1916:14  Interstage sep  -5946 x 120 x 31.9 
 1916:20  LES sep 92 km  -5931 x 122 x 31.9 
 1917:31  T+4:31 SIC apogee, 117 km  
 1918:31  S-II premature CECO 
 1921:07  T+9:07 SIC impact at 30.18N 74.07W 
 1922:53  S-II OECO, sep  -2158 x 190 x 32.6 
   -2160 x 184 x 32.53 (MPR-SAT) 
 1922:57  S-IVB ignition 
 1923:05  Ullage case sep 
 1923:32  SII apogee 191 km  
 1925:30  S-IVB cutoff 
 1925:40  Earth orbit insertion  88.32 184 x 186 x 32.53 
 1933:58  T+20:58 S-II impact 31.32N 33.29W 
 2013   
 2148:46  S-IVB TLI burn 
 2154:37  S-IVB cutoff 
 2154:47  Translunar injection 217 x 566793 x 31.81  
   217 x 535750 x 31.82  
 2219:39  CSM sep from S-IVB/SLA  219 x 549183 x 31.74  
  SLA panels sep 
 2230  CSM docked with LM 
 2232:08  CSM hard docked 
 2314:01  CSM/LM sep from S-IVB 
 2331:01  APS-1 evasive burn 3.0m/s 
 2332:20  APS-1 cutoff  
 2347:39  CVS venting 0.4m/s 
 2352:19  LOX dump 8.7m/s 
 2353:07  LOX dump complete 
 2354:26  H2 NPV vent on 
1970 Apr 12  0113:00  APS-2 burn 9.1m/s  
 0116:36  APS-2 cutoff  25 x 522040 x 31.84  
 1220?  Pass EL1:4 
 1442:10  Unscheduled venting, 2.4m/s  47 x 519381 x 31.832 
1970 Apr 15  0109:40  Impact  

Mars 6

  1973-052A


Mars-6 (3MP No. 50P) successfully delivered its lander to a Mars impact trajectory and flew past the planet in Mar 1974.


Mars-6 
 

DateTimeEventOrbit  

1973 Aug 5  1745:48  Launch by Proton-K  KB 
 1748  Stage 1 sep 
 1751  Stage 2 sep 
 1755  Stage 3 MECO 
 1755  Stage 3 sep  
 1759  Blok D MES-1 
 1801  Blok-D MECO-1 
 1908  Blok-D burn 2, solar orbit 
 1914?  Blok-D MECO-2 
 1914?  Blok-D sep 
1973 Aug 13   TCM 5.3m/s 
1973 Oct   Telemetry system failed 
1974 Feb 24   TCM-2  2.5m/s 
1974 Mar 7  1520?  Enter Mars sphere 
1974 Mar 12  0450  SA sep at 46000 km 
 0900?  Flyby at 1600 km 
1974 Mar 17  0150? Depart Mars sphere 

The lander impacted Mars at 23.9S 19.5 long. at local time 1530, or 0858 UTC.

A delta-V of -116 m/s along the velocity vector is consistent with reducing periapsis from 1600 km to below the surface.

Entry was at 5.60 km/s at 14 deg.

Landed at 23 09S 19 05W (nominal). LT = 12:40.


Mars-6 SA 
 

DateTimeEventOrbit  

1974 Mar 7  1520?  Enter Mars sphere 
1974 Mar 12  0449:16  SA sep, 46000 km   
 0505?  Retrofire 

 

0506?  Retro and truss sep 
 0826:27  Begin velocity data, 4800 km alt 
 0853:40  LOS entry, 75 km (ERT 0906:20, LT=12:40) 
 0854:40  AOS 29 km 
  Drogue motor and drogue sep 
 0855:55  Main parachute deployed
  Aeroshell sep 
  Main parachute sep 
 0858:24  Impact (0911:04 ERT last signal) 

Thursday, April 18, 1996

Molniya 214

  1975-081A


Molniya-2 F14 was launched in Sep 1975,entered the A plane and successfully stabilized its ground track.


Molniya-2 F14 
 

DateTimeEventOrbit  

1975 Sep 9  0019 Launch by 8K78M  PL 
  BVGD sep 
  GO sep 
  T+4:46 Blok A sep 
  T+4:56 KhO sep 
  T+8:46 Blok-I MECO 
 0027 T+8:50 Blok-I sep  
  T+53:16 BOZ burn 
 0112  T+53:56 BOZ sep 
  ML burn 
  T+56:46 ML MECO 
 0115  T+56:54 ML sep   
   736.5 439 x 40837 x 62.8 
1975 Sep 26  717.7 449 x 39902 x 62.9 
1977 Dec 16   end of ops 

Sunday, April 14, 1996

DFH-30

 1990-081A


The second FY satellite was launched in Sep 1990. Mass was 881 kg.

FY-1B temporarily lost attitude control in 1991 because of radiation damage, but control was regained in two months, although lost again later.

The third stage exploded on Oct 4, generating hundreds of debris objects.


Feng Yun 1B 
 

DateTimeEventOrbit  

1990 Sep 3  0053  Launch by CZ-4  T'ai Yuan 
 0055  T+2:31 St 1 MECO 
 0055  T+2:32 St 1 sep 
 0055  T+2:47 Fairing 
 0059  T+6:38 St 2 MECO 
 0059  T+6:48 St 2 VECO 
 0059  T+6:49 St 2 sep 
 0059  St 3 burn? 
  St 3 burn 303s? 
 0103  T+10:10 St 3 MECO 
 0104  T+11:05 St 3 sep  
 0105? Atmosphere sats ejected 
1990 Sep 4    102.77 881 x 897 x 98.9 
1990 Oct 4  2014  Stage 3 exploded 
1991 Feb   Attitude control lost 
1991 Apr   Control regained 
1991?   End of ops 
1992 Mar 20    102.76 878 x 900 x 98.9 

May 13,2026

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