Saturday, January 8, 2000

Pioneer 6

  1965-105A


The first Solar Pioneer, Pioneer A was built by TRW for NASA-Ames. The spin stabilized cylindrical Solar Pioneers would study the solar wind. Pioneer A was launched at 0731:20 by Delta E from Kennedy and became Pioneer VI. The Delta stage separated at 0756:07 and the X-258 ignited at 0756:40 to insert Pioneer into solar orbit. It was still transmitting in 2000, the longest surviving spacecraft. 


Pioneer 6 
 

DateTimeEventOrbit  

1965 Dec 16 0731:21  Launch by Delta E  CK LC17A 
  T+0:43 SRM burnout 
  T+1:10 SRM sep 
 0733:49  T+2:28 Thor S/N 20203 MECO 89 km  
 0733:54  T+2:33s Delta E S/N 20202 burn, 6:18 
  T+2:33s Thor sep  -5343 x 204 x 29.9 
  T+2:59s Fairing 
 0740:12  T+8:51 Delta SECO 
 0756:07  T+24:46 St 3 spinup 
 0756:09  Delta sep  273 x 1267 x 30.2 
 0756:18  X-258-C4 RH-90 burn, 23s 
 0756:42  X-258 burnout 
 0757:42? X-258 sep 
 0757  Deploy booms  558 x -291986 x 30.23 
1965 Dec 26?   Solar orbit (1Mkm) 
1975   Last data to be archived 
1988 Oct   Passed 3Mkm from Earth 
1997 Oct 6   Plasma and cosmic ray data OK 
2000 Dec 8   Telemetry received in anniversary contact 

Thursday, January 6, 2000

Kosmos 1451

 1983-029A


Two-tone telemetry; Hi res satellite


Kosmos-1451 
 

DateTimeEventOrbit  

1983 Apr 8  0930 Launch by Soyuz-U  Plesetsk 
 0934Blok-I burn 
 0938Blok-I sep 
1983 Apr 8    88.73 183x237x82.35 
1983 Apr 9    90.04 227x323x82.35 
1983 Apr 18    90.09 236x319x82.35 
1983 Apr 21    90.02 234 x 315 x 82.4 
1983 Apr 22   
 0504? Deorbit 
 0514? PO sep 
 0521? Entry 
 0536? Landed 

Sunday, January 2, 2000

STS-68 (Endeavour)

 1994-062A


The STS-68 mission had an RSLS abort at T-1.9s on 1994 Aug 18 due to higher than expected temperatures on engine 2032. The launch was postponed until after the STS-64 flight. The second Space Radar Lab mission finally got off the ground at 1115.58 UT on 1994 Sep 30. SRB separation was at 0718 and MECO and ET separation came at 0724, leaving Endeavour in a 52 x 213 km x 57 deg orbit. The OMS 2 circularization burn was at MET 35:10, or 0751 UT. The orbit at Sep 30.70 was 213 x 226 km x 57.0 deg.

Trim burns were made on Oct 4 to adjust the orbit to match that of the STS-59 flight to within 10 meters. The orbit was lowered on Oct 7 for an interferometry experiment. A trim burn on Oct 9 adjusted the orbit again. 

STS-68 
Date  Time  Event  Orbit 
1994 Jul 21   Tow to VAB 
1994 Aug 3 Rollout 
1994 Aug 18  1053:58  RSLS abort T-1.8s  LC39 
1994 Aug 24   Rollback  VAB 
1994 Sep 30  1116:00  Launch  LC39 
 1118:04  SRB sep T+2:04 
 1124:35  MECO T+8:35  87.24 49 x 226 x 57.0 (OMS dV) 
 1124:54  ET sep  52 x 213 x 57.0  
 1126:35  Prop dump 
 1151:09  OMS-2 1:39 49m/s 88.90 214 x 226 x 57.01 
 1249  PLBD open 
  Activate radar 
1994 Oct 2    88.86 212 x 224 x 57.0 
1994 Oct 5    88.80 209 x 221 x 57.0 
1994 Oct 7  0600   88.76 206 x 219 x 57.0 
  Lower orbit 
1994 Oct 81600   88.61 199 x 212 x 57.0 
1994 Oct 10 Deactivate radar payload 
1994 Oct 11  0600   88.60 198 x 211 x 57.0 
 1206  PLBD closed 

1607:19  Deorbit 2:18 73m/s  -42 x 210 x 57 
 1629:46  Entry interface 
 1702:09  Landed  RW22 EAFB 
 1702:11  Drag chute 
 1702:21  NGTD 
 1703:10  Wheels stop 

Booklist: December 15,1999

 https://welib.org/md5/e1f604f46f3d96e0e16c586b76ecaa56

May 13,2026

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