Concept Evaluation of Four Thermal Utility Systems for Low Orbit Spacecraft
- 11 July 1983
- proceedings article
- Published by SAE International in SAE International Journal of Advances and Current Practices in Mobility
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Development of a double-wall artery high capacity heat pipePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Military spacecraft thermal management - The evolving requirements and challengesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- A pumped, two-phase flow heat transport system for orbiting instrument payloadsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981