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RS D1, D2 (Rohini 2, 3)
RS D1 [ISRO]
The third and fourth satellites in the Rohini program, called RS D1 and D2 (Rohini satellite) were small satellites to test simple earth observation payload.
The spin-stabilized 35 kg satellites featured launch earth observation instruments and were powered by body monted solar cells.
RS D1 featured a remote sensing payload called Landmark Tracker. Due to too low orbit, the satellite reentered premature after only 9 days.
RS D2 had a Smart sensor remote sensing payload, which had both visible and infra-red capabilites. The mission operated for 17 months.
| Nation: | India |
|---|---|
| Type / Application: | Technology, earth observation |
| Operator: | ISRO |
| Contractors: | ISRO |
| Equipment: | |
| Configuration: | |
| Propulsion: | |
| Power: | Solar cells, batteries |
| Lifetime: | 9 days (#D1); 1.5 years (#D2) |
| Mass: | 38 kg (#D1); 41.5 kg (#D2) |
| Orbit: | 186 km × 418 km, 46° (#D1); 371 km × 861 km, 46° |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| RS D1 (Rohini 2) | 1981-051A | 31.05.1981 | Sr | P | SLV-3 | |
| RS-D2 (Rohini 3) | 1983-033A | 17.04.1983 | Sr | SLV-3 |
Further Rohini missions:
