Analysis of sprays from rocket engine injectors
- 1 July 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (7) , 796-798
- https://doi.org/10.2514/3.30321
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Effect of orifice length-to-diameter ratio on mixing in the spray from a pair of unlike impinging jetsJournal of Spacecraft and Rockets, 1970
- A closed-form solution for minimum-fuel, constant-thrust trajectoriesAIAA Journal, 1970
- An experimental technique for measurement of injector spray mixingJournal of Spacecraft and Rockets, 1969
- Mixture ratio distribution - Its impact on rocket thrust chamber performance.Journal of Spacecraft and Rockets, 1967