Space tether missions — различия между версиями
Материал из Department of Theoretical and Applied Mechanics
| Строка 22: | Строка 22: | ||
|30 m | |30 m | ||
|30 m | |30 m | ||
| − | | | + | |3800 kg |
| − | | | + | |3200 kg |
|296 km | |296 km | ||
|28.85° | |28.85° | ||
| − | | | + | |Два спутника, связанные тросом, приведены во вращение для достижения искусственной гравитации (0.00015 g) |
|[http://en.wikipedia.org/wiki/Gemini_11] | |[http://en.wikipedia.org/wiki/Gemini_11] | ||
|- | |- | ||
| Строка 34: | Строка 34: | ||
|20 km | |20 km | ||
|260 m | |260 m | ||
| + | |12200 kg | ||
| | | | ||
| − | |||
|430 km | |430 km | ||
|28.5° | |28.5° | ||
| Строка 46: | Строка 46: | ||
|20.7 km | |20.7 km | ||
|19.7 km | |19.7 km | ||
| + | |10600 kg | ||
| | | | ||
| − | |||
|296 km | |296 km | ||
|28.5° | |28.5° | ||
Версия 20:14, 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 | 3800 kg | 3200 kg | 296 km | 28.85° | Два спутника, связанные тросом, приведены во вращение для достижения искусственной гравитации (0.00015 g) | [1] |
| Shuttle TSS-1 | 1992 | M | 20 km | 260 m | 12200 kg | 430 km | 28.5° | [2] | ||
| Shuttle TSS-1R | 1996 | M | 20.7 km | 19.7 km | 10600 kg | 296 km | 28.5° | [3] |
