Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.
SROSS C, C2
SROSS C [ISRO]
SROSS C and C2 (Stretched Rohini Satellite Series) were the third and fourth satellites in ISRO's SROSS series and to perform experiments on Gamma-ray astronomy and ionospheric science.
The satellite body was spin-stabilized. A Hydrazine based monopropellant reaction control system was also fitted. Power was to be provided by body mounted solar cells.
The satellites carried two payloads:
- 20 - 3000 keV Gamma-ray Burst Experiment (GRB)
- Retarding Potential Analyser (RPA)
SROSS C was launched into a lower than planned orbit and therefore had a significantly reduced lifetime. It decayed from orbit on 14 July 1992 after only 55 days.
SROSS C2 was launched successfully and operated for four years.
| Nation: | India |
|---|---|
| Type / Application: | Technology, science |
| Operator: | ISRO |
| Contractors: | ISRO |
| Equipment: | GRB, RPA |
| Configuration: | |
| Propulsion: | Hydrazine RCS |
| Power: | Solar cells, batteries |
| Lifetime: | 6 months (planned); 55 days (reached, #C); 4 years (reached, #C2) |
| Mass: | 106 kg (#C); 115 kg (#C2) |
| Orbit: | 267 km × 391 km, 45° (#C); 430 km × 600 km, 45° (#C2) |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| SROSS C | 1992-028A | 20.05.1992 | Sr | P | ASLV | |
| SROSS C2 | 1994-027A | 04.05.1994 | Sr | ASLV |
References:
- ISRO: SROSS C
- ISRO: SROSS C2
- NASA HEASRC: Stretched Rohini Satellite Series (SROSS) 3 & C2
Further Rohini missions:
