Orbital transfer and release of tethered payloads. Continuation of investigation of electrodynamic stabilization and control of long orbiting tethers Martinez-Sanchez, Manuel
Abstract
The effect of reeling operations on the orbital altitude of the tether system and the development of control laws to minimize tether rebound upon payload release were studied. The use of the tether for LEO/GEO payload orbital transfer was also investigated. It was concluded that (1) reeling operations can contribute a significant amount of energy to the orbit of the system and should be considered in orbit calculations and predictions, (2) deployment of payloads, even very large payloads, using tethers is a practical and fully stable operation, (3) tether augmented LEO/GEO transfer operations yield useful payload gains under the practical constraint of fixed size OTV's, and (4) orbit to orbit satellite retrieval is limited by useful revisit times to orbital inclinations of less than forty-five degrees.
- Publication:
-
Smithsonian Astrophysical Observatory Report
- Pub Date:
- March 1983
- Bibcode:
- 1983sao..rept.....C
- Keywords:
-
- Dynamic Characteristics;
- Electrodynamics;
- Payload Retrieval (Sts);
- Reels;
- Tethered Satellites;
- Transfer Orbits;
- Altitude;
- Computerized Simulation;
- Space Maintenance;
- Launch Vehicles and Space Vehicles