Thursday, August 9, 2007

SRE

 2007-001C


The ISRO Space Recovery Experiment had a mass of 555 kg; launch with Cartosat-2 on PSLV-C7. It carried microgravity experiments and was recovered in the ocean. It uses Agni components.

Deorbit 160m/s by liquid engine. Orbit 490 x 635 km x 97 deg. Entry at 100.7km 7.962 km/s at an angle of -2.4 deg. Splashdown 140 km E of Sriharikota, in Bay of Bengal near 13.3N 81.4E

Rounded cone 2.0m dia 1.6m h. Engine has 8 x 22N thrusters.


SRE-1 
 

DateTimeEventOrbit  

2007 Jan 10 0353 Launch by PSLV-C7  SDSC 
  T+0:25 PSOM 3-4 on 
  T+1:08 PSOM 1-2 sep 
  T+1:30 PSOM 3-4 sep 
  T+1:53 Stage 1 sep 
  T+1:53 Stage 2 on 
  T+2:39 Fairing 
  T+4:24 PS2 sep 
  T+4:25 PS3 on 
  T+8:38 PS3 sep, 504 km  
  T+8:53 PS4 on, 516 km  
  T+15:49 PS4 off, 639 km 
  T+16:06 Cartosat sep 
  T+17:11 DLA-U (Dual Launch Adapter) sep 
  with Pehuensat 
  T+18:26 SRE-1 sep 
2007 Jan 10    97.32 620 x 640 x 97.9 
2007 Jan 15    97.31 618 x 641 x 97.9 
2007 Jan 16   Orbit tweak 97.35 620 x 642 x 97.9 
2007 Jan 20   D-2d orbit change to Repetitive Elliptical Orbit  95.81 478 x 637 x 97.9  
2007 Jan 22  0312  Reorient for deboost  95.95 486 x 642 x 97.9 
 0330  Deorbit at 625 km, 9:19  
 0340  Deorbit MECO -42 x 649 x 97.9  
 0347  Orient for entry 
 0407  D+36:19 Entry 8.04km/s at 100 km  
  D+42:24 Pilot and drogue chute deploy, 5 km 
  D+43:20 Main chute deploy, 2 km  
 0417  D+46:00 Splashdown, 12m/s 
 0520  Capsule located 

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