Sunday, June 20, 2010

Navstar 62

 2010-022A


SVN62 was Block IIF SV-1, PRN 25, Plane B.

The GPS Block IIF satellites are to replace the Block IIR. Block IIF has a civilian L5 channel. [249] The initial contract was for 6 satellites from Rockwell/Seal Beach; manufacturing was transferred to Boeing/El Segundo in 2001.

Boeing/ES satellite. Mass 1630 kg launch (MOB). Size 2.5 x 2.0 x 1.8m +box + 2 panels. IIF solar array deplyed 7.8m each; estimate 18m span.

Launch by EELV in 2008.


GPS 
 

DateTimeEventOrbit  

2010 May 28 0300:00 Launch by Delta 4M+(4,2)  CC SLC37B 
  Az 105.28deg 
  T+1:34 GEM60 SRM burnout  
  T+1:40 SRM sep 
  T+4:05 MECO 
  T+4:11 CBC sep 
  T+4:26 Stage 2 SES-1 
  T+4:36 Payload fairing sep
 0312 T+12:11 SECO-1  185? x 200? x 37.5?  
  S Eq crossing 32W 
 0321 T+21:17 SES-2 
 0324:00  243 km Vrel 9.173km/s  245 x 14500 x 36? 
  T+24:34 SECO-2  245? x 20459 x 43.90? 
   358.6 237 x 20450 x 43.3 (UN) 
 0620 T+3:20:44 SES-3 
  T+3:22:22 SECO-3  20459 x 20459 x 55 
  T+3:28:53 Spinup 
 0633 T+3:33:03 GPS sep from Delta 
  T+3:48:00? Begin blowdown stage 2 
  T+4:00:00? Stage 2 disposal burn complete 20400 x 21500 x ? 
   754.1 20462 x 21679 x 54.7 (UN, B)  

Payload:

  • L1M link 1575.42 MHz, military code + civil?

  • L2M link 1227.6 MHz, military code

  • L2C civil link

  • L5 civil channel 1176 MHz

  • L3 Nuclear detection data return

  • L4 classified experiment

  • DASS Distress Alert Satellite System, MEOSAR development

  • CXD energetic particle sensor

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