Performance and flow calculations for a gaseous H2/O2 thruster
- 1 July 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 28 (4) , 433-438
- https://doi.org/10.2514/3.26263
Abstract
No abstract availableKeywords
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