The results are presented of studies performed relating to the feasibility of deploying a subsatellite from the shuttle by means of a tether. The dynamics, the control laws, the aerodynamics, the heating, and some communication considerations of the tethered subsatellite system are considered. Nothing was found that prohibits the use of a subsatellite joined to the shuttle by a long (100 km) tether. More detailed studies directed at specific applications are recommended.
Tethered subsatellite study
1976-03-01
Report
Keine Angabe
Englisch
NTIS | 1976
|Optimal control of the Shuttle-Tethered-Subsatellite system
Elsevier | 1980
|Optimal Trajectories for Deployment/Retrieval of Tethered Subsatellite
British Library Conference Proceedings | 1996
|Tracking Control of Tethered Subsatellite through an Optimal Path
British Library Conference Proceedings | 1994
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