Fluid dynamic effects on Apollo engine pressure spikes.
- 1 January 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 5 (1) , 31-35
- https://doi.org/10.2514/3.29181
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Environmental effects upon rocket injector/ chamber compatibility.Journal of Spacecraft and Rockets, 1967