Internal ballistic considerations in hybrid rocket design.
- 1 February 1967
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 4 (2) , 255-262
- https://doi.org/10.2514/3.28844
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Regression rates of metalized hybrid fuel systems.AIAA Journal, 1966
- Combustion in the turbulent boundary layer on a vaporizing surfaceSymposium (International) on Combustion, 1965
- Regression rates of nonmetalized hybrid fuel systemsAIAA Journal, 1965
- Regression rates and the kinetics of polymer degradationSymposium (International) on Combustion, 1965
- Fundamentals of Hybrid Boundary-Layer CombustionPublished by Elsevier ,1964
- Introductory Considerations on Hybrid Rocket CombustionPublished by Elsevier ,1964
- TURBULENT BOUNDARY LAYER COMBUSTION IN THE HYBRID ROCKETPublished by Elsevier ,1963