Space tether missions — различия между версиями
Материал из Department of Theoretical and Applied Mechanics
| Строка 24: | Строка 24: | ||
| | | | ||
|3.8 kg | |3.8 kg | ||
| − | | | + | |296 km |
| − | | | + | |28.85° |
| | | | ||
|[http://en.wikipedia.org/wiki/Gemini_11] | |[http://en.wikipedia.org/wiki/Gemini_11] | ||
Версия 19:41, 19 февраля 2012
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 | Atitude | Inclination | Comments | Links |
|---|---|---|---|---|---|---|---|---|---|---|
| Gemini 11 | 1966 | M | 30 m | 30 m | 3.8 kg | 296 km | 28.85° | [1] | ||
| Shuttle TSS-1 | 1992 | M | 20 km | 260 m | 12.2 kg | 430 km | 28.5° | [2] | ||
| Shuttle TSS-1R | 1996 | M | 20.7 km | 19.7 km | 10.6 kg | 296 km | 28.5° | [3] |
