Optimum exhaust velocity for laser-driven rockets
- 1 November 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 12 (11) , 700-701
- https://doi.org/10.2514/3.27867
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Comparison of Advanced Propulsion Concepts for Deep Space ExplorationJournal of Spacecraft and Rockets, 1972
- Regression rates of nonmetalized hybrid fuel systemsAIAA Journal, 1965
- Fundamentals of Hybrid Boundary-Layer CombustionPublished by Elsevier ,1964
- TURBULENT BOUNDARY LAYER COMBUSTION IN THE HYBRID ROCKETPublished by Elsevier ,1963