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New functional approaches for redundant inert gas thruster systems
- Source :
- AIAA Guidance, Control, and Flight Mechanics Conference.
- Publication Year :
- 1969
- Publisher :
- American Institute of Aeronautics and Astronautics, 1969.
-
Abstract
- Valving concepts and functional approaches for inert gas attitude control thrustor systems providing redundancy safeguards at minimum weight, volume and power costs
Details
- Database :
- OpenAIRE
- Journal :
- AIAA Guidance, Control, and Flight Mechanics Conference
- Accession number :
- edsair.doi...........3a936264504391a5be137792b18aa922