Performance Calculations for Hybrid Nuclear-Chemical Rocket Propulsion Systems
- 1 March 1959
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in ARS Journal
- Vol. 29 (3), 180-186
- https://doi.org/10.2514/8.4715
Abstract
No abstract availableKeywords
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- Some Mechanical Properties of Graphite at Elevated TemperaturesJournal of Applied Physics, 1951
- Maintenance of Near Equilibrium during Isentropic Expansions through a NozzleJournal of the American Chemical Society, 1949
- Chemical Reaction During Adiabatic Flow through a Rocket NozzleThe Journal of Chemical Physics, 1949
- Recombination of Hydrogen Atoms. IIIJournal of the American Chemical Society, 1938