A transpiration-cooled nozzle as applied to a gas-core nuclear propulsion system
- 1 May 1965
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 2 (3) , 345-353
- https://doi.org/10.2514/3.28182
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
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