Simplified thermal fatigue analysis for liquid rocket combustion chambers.
- 1 January 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 4 (1) , 126-128
- https://doi.org/10.2514/3.28824
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- OPTIMAL PROGRAMMING PROBLEMS WITH INEQUALITY CONSTRAINTSAIAA Journal, 1963
- Optimum Rocket Trajectories With Aerodynamic DragJournal of Jet Propulsion, 1958
- Optimum Thrust Programming for a Sounding RocketJournal of the American Rocket Society, 1951