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 | ||
| + | !Perigee | ||
| + | !Apogee | ||
| + | !Inclination | ||
| + | !Period | ||
!Comments | !Comments | ||
!Links | !Links | ||
| Строка 30: | Строка 34: | ||
|20 km | |20 km | ||
|260 m | |260 m | ||
| − | | | + | |82.5 kg |
| − | | | + | |12.2 kg |
| + | |425 km | ||
| + | |437 km | ||
| + | |28.5° | ||
| + | |93.2 min | ||
| | | | ||
|[http://en.wikipedia.org/wiki/STS-46] | |[http://en.wikipedia.org/wiki/STS-46] | ||
| Строка 42: | Строка 50: | ||
| | | | ||
|10.6 kg | |10.6 kg | ||
| + | |277 km | ||
| + | |320 km | ||
| + | |28.5° | ||
| + | |93.5 min | ||
| | | | ||
|[http://en.wikipedia.org/wiki/STS-75] | |[http://en.wikipedia.org/wiki/STS-75] | ||
Версия 19:24, 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 | 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] |
