
Astro B [ISAS]
The Astro B (renamed Tenma after launch) X-ray astronomy mission had the following major objectives:
The spacecraft could spin at 0.546, 0.137, or 0.068 rpm with the aid of a momentum wheel. The spin axis was maneuvered by magnetic torquing.
Four experiments were on board of the satellite:
| Nation: | Japan |
|---|---|
| Type / Application: | Astronomy, X-Ray |
| Operator: | ISAS |
| Contractors: | |
| Equipment: | see above |
| Configuration: | |
| Propulsion: | |
| Power: | 4 deployable fixed solar arrays, batteries |
| Lifetime: | |
| Mass: | 216 kg |
| Orbit: | 489 km × 503 km, 31.5° |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| Astro B (Tenma) | 1983-011A | 20.02.1983 | Ka LP-M | M-3S |
