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Last updated on: 30-Aug-2017
STRETCHED ROHINI SATELLITE SERIES-1
| Application | Experimental |
| Lift-off Mass | 150 kg |
| Spacecraft Power | Solar Array: 90 Watts Batteries:Ni-Cd (12 Ah) |
| Communication | S band and VHF Band |
| Stabilization | Three axis body or spin stabilized using momentum wheels & reaction control systems. Sensors: Magnetometer, Twin-slit sun sensor and conical earth sensor. RCS: Monopropellant |
| Payload | Launch Vehicle Monitoring Platform(LVMP), Gamma Ray Burst (GRBE) Experiment & Corner Cube Retro Reflector (CCRR) for laser tracking |
| Launch Date | March 24, 1987 |
| Launch Vehicle | ASLV-1 (Orbit not achieved) |
| Achievements | First developmental flight of ASLV |