Space tether missions — различия между версиями
Материал из Department of Theoretical and Applied Mechanics
| Строка 12: | Строка 12: | ||
!Mass 1 | !Mass 1 | ||
!Mass 2 | !Mass 2 | ||
| − | ! | + | !Atitude |
| − | |||
!Inclination | !Inclination | ||
| − | |||
!Comments | !Comments | ||
!Links | !Links | ||
| Строка 24: | Строка 22: | ||
|30 m | |30 m | ||
|30 m | |30 m | ||
| + | | | ||
| + | |3.8 kg | ||
| | | | ||
| | | | ||
| Строка 34: | Строка 34: | ||
|20 km | |20 km | ||
|260 m | |260 m | ||
| − | | | + | | |
|12.2 kg | |12.2 kg | ||
| − | | | + | |430 km |
| − | |||
|28.5° | |28.5° | ||
| − | |||
| | | | ||
|[http://en.wikipedia.org/wiki/STS-46] | |[http://en.wikipedia.org/wiki/STS-46] | ||
| Строка 50: | Строка 48: | ||
| | | | ||
|10.6 kg | |10.6 kg | ||
| − | | | + | |296 km |
| − | |||
|28.5° | |28.5° | ||
| − | |||
| | | | ||
|[http://en.wikipedia.org/wiki/STS-75] | |[http://en.wikipedia.org/wiki/STS-75] | ||
Версия 19:39, 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 | [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] |
