Friday, September 8, 1972

Saturn S-IVB-511

  1972-031B


SA-511 was launched on 1972 Apr 16 at 1754 UTC.

After CSM sep, the LH2 dump was nonpropulsive. The LOX dump Apr 16 at 2233 UTC to 2234 UTC gave an 8m/s velocity change.

The S-IVB-511 stage impacted the lunar surface at 2102:04 on Apr 19 at location 2.1N 22.1W with velocity of 2.655 km/s at an impact angle of 16.6 deg.


S-4B-511 
 

DateTimeEventOrbit  

1972 Apr 16  1754  Launch  
 2212  APS evasive 80s 
 2212  CVS vent 
 2217  CVS vent complete 
 2233  LOX dump 48s 8m/s 
 2334  APS targeting 54s 2.5m/s 
   147 x 451211 x 32.5 
1972 Apr 19  2102:03 Lunar impact  -119 x Inf x 14? 

Monday, August 21, 1972

Explorer 13

 1961-022


The second in the series, S-055A, reached orbit on 1961 Aug 25. Ascent was at an 80 degree elevation and 90 deg (eastward) azimuth. However, the orbit was lower than planned, 125 x 1164 km x 37.7 deg, due to a large injection angle error. (TN-D-1396 indicates initial perigee was 139 km, with an injection angle of -4.396 degrees; injection altitude was 455.6 km, so injection velocity was around 7.748 km/s). 

The S-55 satellite was attached to the Altair X-248-A5 stage and a set of pressurized cells was installed around the rocket stage. Mass was 57 kg payload; 86 kg including the 22 kg empty Altair and upper 'D' Scout section, which was 6 kg. Size was 1.93m long 0.58m dia. LaRC managed the project, with detectors from LaRC, LeRC and GSFC.


Explorer 13 
 

DateTimeEventOrbit  

1961 Aug 25  1829:44  Launch by Scout ST-6  WI 
  T+0:42 St 1 Algol burnout 1.1 km/s 15 km 
  T+1:14 St 1 sep 
  T+1:14 St 2 Castor burn 38 km 0.9 km/s 
 1831:41 T+1:57 St 2 burnout 76 km 2.7 km/s  
  T+1:57 St 3 heat shield sep  
 1831:59 T+2:15 Fairing sep 107 km 
 1831:59 St 2 sep  
 1831:59 T+2:15 St 3 Antares burn, 107 km 2.7 km/s 
 1832:36 T+2:52 St 3 burnout 
  Coast 
 1837:46 Spinup to 190 rpm
 1837:48 T+8:04 St 3 sep 
 1837:48 T+8:04 St 4 Altair burn 453 km 
 1838:29 T+8:45 St 4 burnout  

1961 Aug 25  

 (Minitrack)  113 x 1147 x 37.7 
1961 Aug 26    97.5 125 x 1164 x 37.7 
1961 Aug 28   Reentered 

Payload:

  • X-248A5 motor

  • Langley pressurized cell detector (five rows of 32 cells each, outside X-248)

  • LeRC Grid detector (60), aft section

  • GSFC Cu wire card detector (46), aft section

  • LaRC Impact detector (2), nose section

  • Solar cell experiments, nose section 

Thursday, June 22, 1972

ESSA 6

  1967-114A


TOS D, the third operational APT satellite, was renamed ESSA VI after its successful launch on 1967 Nov 10 frm Vandenberg. The Delta E1 launch vehicle put ESSA VI in a 1410 x 1488 km x 102.1 deg orbit and it was declared operational on Nov 22. Two years later it was noted that the vidicon cameras had degraded and that the satellite had drifted out of sun-synchronous orbit. ESSA VI was decommissioned on 1969 Dec 12.


ESSA 6 
 

DateTimeEventOrbit  

1967 Nov 10  1753:08  Launch by Delta E1  V SLC2E 
 1755  T+2:30 Thor S/N 20222 MECO 
 1755  Delta S/N 20221 burn 6:18 
 1801? Delta SECO 
 1811  Equator crossing 
 1811? FW-4D S/N 41105 burn 30s 
 1811? FW-4D burnout  1410 x 1488 x 102.1 
 1813? FW-4D sep 
 1813? Despin 
1967 Nov 22   Operational 
1969 Dec 12   Decommissioned 

November 20,2006

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