This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Thermal Control of the Tethered Satellite Module
Annotation ability available
Sector:
Language:
English
Abstract
This paper deal with the thermal design features of the Tethered Satellite Module, according to the project development status of the advanced Phase B. A description of TSM typical mission characteristics, thermal requirements and constraints and the proposed thermal control design will be given. The thermal analytical models, the subsystem performances and the more representative temperature predictions will be presented with emphasis to special features which may occur.
Authors
Topic
Citation
Borriello, G. and Pellis, G., "Thermal Control of the Tethered Satellite Module," SAE Technical Paper 831138, 1983, https://doi.org/10.4271/831138.Also In
References
- Laue J.H. Manarini F. “The Tethered retrievable platform concept and utilization” IAF-82-13
- Borriello G. et al. “Thermo-dynamic analysis for altitudes of 100-120 km” Aeritalia Report TS-RP-AI-009, dated 10.1.83 “Thermal Control of Tethered satellite during very low altitude aerodynamic mission” Paper to be submitted to CNS/ESA International Symposium: “Environmental and thermal control systems for space vehicles” 4-7 October 1983
- Oppenheim A.K. “Generalized theory of convective heat transfer in a free-molecular flow” Journal Aerosp. Sci. 1953
- Borriello G. Chiarelli C. “Thermal behaviour and control of TSM RCS subsystem” Aeritalia Technical Note TS-TN-A1-015 2 20 4 83