Saturday, March 15, 1997

Luna 4A

  1963-001B


The first E-6 was E-6 No. 2 (No. 1 was a ground test article). It was launched on 1963 Jan 4. It used the first 8K78L rocket, a version of the 8K78 whose upper two stages were guided by a control system on the E-6 payload. It reached orbit, but the Blok-L stage did not ignite. The BOZ ullage unit failed to operate because of a power system failure and the I-100 control unit on the E-6 failed to send the ignition command to the Blok-L. Three objects were tracked; object 01A (SATCAT 521) is thought to have been the Blok-I stage, and reentered in a day. Object 01B (SATCAT 522) is usually listed as the E-6 probe with object 01C as debris; however 01C seems to have decayed more slowly. An alternate possibility is that 01C was the E-6 and Blok-L (still attached) while 01B was the BOZ unit.


E-6 No. 2 
 

DateTimeEventOrbit  

1963 Jan 4  0849 Launch by Molniya  KB 
 0854  Blok-A sep 
 0854  Blok-I burn 
 0858  Blok-I sep 
 0949? BOZ failed 
 1009  01A 88.04 165 x 189 x 64.6 (A) 
 1900  01B 88.40 164 x 226 x 64.6 (B) 
1963 Jan 5   01A reentered 
1963 Jan 7  0300  01B  88.23 178 x 194 x 64.8 
1963 Jan 7  0304  01C  88.55 178 x 226 x 64.8 
1963 Jan 9  0301  01B  87.98 174 x 174 x 64.8 
1963 Jan 10  0447  01C  88.32 163 x 219 x 64.7 
1963 Jan 11   01B reentered 
1963 Jan 16  01C reentered 

Market Driven Menus

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Friday, March 14, 1997

MSTI-2

 1994-028A


MSTI 2 was built by Spectrum Astro for USAF Phillips Lab using the SA200S series bus. This added a hydrazine propulsion system to the MSTI-1 vehicle. The 168 kg octagonal box-shaped, 3-axis stabilized satellite was designed for theater ballistic missile acquisition and tracking, and was originally intended to watch tests of the LEAP projectile. It observed a Minuteman launch from Vandenberg in Jun 1994.


MSTI 2 
 

DateTimeEventOrbit  

1994 May 9  0247  Launch by Scout G-1  V SLC5 
  T+1:24 Stage 1 burnout 
  T+1:28 St 1 sep 
  T+1:28 St 2 burn 
  T+2:09 St 2 burnout 
  T+2:20 Fairing sep 
  T+2:22 St 2 sep, St 3 burn 
  T+3:10 St 3 burnout 
  T+10? St 3 sep 
 0257? T+10? St 4 burn 
 0257? T+10? Stage 4 burnout 
 0304  T+17 min Star 20 sep, in orbit 
   360 x 461 x 96.8 
1994 Jun 8  1630Observed VAFB Minuteman launch 

DFH-33

 1990-089A


FSW-1 No. 3 was launched in Oct 1990. Mass was 2080 kg. This flight carried guinea pigs and as far as is known was the first flight by the Chinese which carried animals.


FSW 1 
 

DateTimeEventOrbit  

1990 Oct 5  0614  Launch by CZ2  JQ 
 0616  T+2:10 MECO 
 0616  Stage 2 burn 
 0618?  T+4:02? Stage 2 MECO 
 0621?  Stage 2 VECO 
 0621? CZ-2C sep 89.72 208 x 312 x 57.0 
1990 Oct 6  0111   89.69 208 x 309 x 57.0 
1990 Oct 12  1652   89.45 203 x 291 x 57.0 
1990 Oct 13  0342? Capsule sep 
1990 Oct 13  0352? Capsule recovered 
1990 Oct 13  0617   89.47 203 x 293 x 57.0 
 1813   89.46 199 x 295 x 57.0 
1990 Oct 16  1400   89.15 193 x 271 x 57.0 
1990 Oct 20   End of transmissions (RAE) 
1990 Oct 22  1400   87.68 148 x 171 x 57.0

May 13,2026

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