Saturday, October 10, 1992

Gambit 1

  1963-028A


The first KH-7 GAMBIT flight, SV 951, was launched in Jul 1963 by Atlas Agena D from the Point Arguello Naval Missile Facility adjacent to Vandenberg. The spacecraft remained attached to the Agena D for the first day, when the RV was recovered. The Agena gas was depleted after 9 orbits resulting in the vehicle becoming unstable and SRV recovery was done via the emergency Lifeboat system on rev 18. According to the AFCRL data the cosmic radiation package in the SRV was successfully recovered. The recovered reconnaissance film was out of focus but had a best resolution of 1 meter, much better than any previous spy satellite imagery.

After recovery, OCV then separated from the Agena 4702 upper stage in a test of the stabilization system, and reentered after 5 days on around Jul 18.0. OCV remained stable to orbit 25, was then deactivated and on orbit 34 reactivated, although it then was affected by spurious commands.

It isn't clear how long after SRV recovery the OCV separation happened; in the table below I assume it was one orbit later, but it may have been immediate. Similiary, SRV recovery times are not known exactly, and may be in error by one orbit even when a specific revolution is noted because of ambiguity in numbering of revolutions.



KH-7 1 
 

DateTimeEventOrbit  

1963 Jul 12  2045:59  Launch by Atlas Agena D  NMFPA 
 2048:17  BECO (T+2:18) 
 2050:36  SECO (T+4:37) 
 2050:53  VECO (T+4:54) 
 2050:58  Atlas sep (T+4:59) 
 2051:50  Agena burn (T+5:51) 
 2055:38  Agena MECO (T+9:39)  88.51 208 x 213 x 95.35 (VCR)  
1963 Jul 13  0801   88.34 173 x 211 x 95.3 
1963 Jul 13   Rev 15 last image 
1963 Jul 13  2315?  RV sep 
1963 Jul 13  2330?  RV recovered on Rev 18 
1963 Jul 14  0050?  OCV sep from Agena D 
1963 Jul   OCV orbit (28A) 88.3 173 x 212 x 95.3 (SATCAT) 
  Agena 4702 orbit (28C) 88.1 176 x 185 x 95.4 (SATCAT) 
  Debris orbit (28B)  87.8 122 x 216 x 95.3 (SATCAT) 
1963 Jul 16   Agena 4702 reentered 
1963 Jul 17  0200 OCV orbit  164 x 164 x 95.37 (RAE) 
1963 Jul 17  0315 87.76 163 x 163 x 95.4 
1963 Jul 17   OCV SV 951 reentered after 5.2d 

Friday, October 9, 1992

CAT-2

 1980-F01


The CAT capsule on the second Ariane launch, LO2, had a mass of 334 kg. It was similar to CAT 01, with a conical adapter above the cylindrical CAT module, but apparently without the ballast. Above CAT was a further cylinder with a transverse tube on which was mounted AMSAT, hanging off one side.

The Ariane was destroyed less than two minutes after launch from Kourou when the first stage engines shut down early. LO2 was targeted to a 17.5 deg trajectory for better tracking; the yaw manuever at T+2:41 changes the azimuth from 93.5 deg to 110.5 deg. At the time of the failure, before this yaw, the inclination was probably around 6.0 deg.


CAT 2 
 

DateTimeEventOrbit  

1980 May 23  1429:39 Launch by Ariane LO2  CSG ELA1 
 1429:43  T+4s Engine D pressure fluctuation 
 1429:45  T+6s all normal 
 1430:07  T+28s Engine D pressure fluctuation 
 1430:47  T+64s roll torque 
 1431:23  T+104s roll at 60 deg per second 
 1431:27  Self-destruct T+108s, 30 km

May 13,2026

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