Space tether missions
Материал из Department of Theoretical and Applied Mechanics
Версия от 19:24, 19 февраля 2012; Антон Кривцов (обсуждение | вклад)
Comparison of the parameters for the known Space tether missions
Types of the missions: H — Human Space missions, S — Satellite missions, R — Rocket flights (not orbiting).
| Mission | Year | Type | Length total |
Length deployed |
Mass 1 | Mass 2 | Perigee | Apogee | Inclination | Period | Comments | Links |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Gemini 11 | 1966 | M | 30 m | 30 m | [1] | |||||||
| Shuttle TSS-1 | 1992 | M | 20 km | 260 m | 82.5 kg | 12.2 kg | 425 km | 437 km | 28.5° | 93.2 min | [2] | |
| Shuttle TSS-1R | 1996 | M | 20.7 km | 19.7 km | 10.6 kg | 277 km | 320 km | 28.5° | 93.5 min | [3] |
