Limitations on gaseous nuclear rocket I sub sp due to nozzle coolantrequirements.
- 1 October 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 3 (10) , 1515-1522
- https://doi.org/10.2514/3.28687
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- A transpiration-cooled nozzle as applied to a gas-core nuclear propulsion systemJournal of Spacecraft and Rockets, 1965
- Composite Thermal Protection Systems for Manned Re-Entry VehiclesARS Journal, 1962
- Experimental Evaluation of Heat Transfer with Transpiration Cooling in a Turbulent Boundary Layer at M = 3.2Journal of the Aerospace Sciences, 1960
- Experiments on Porous-Wall Cooling and Flow Separation Control in a Supersonic NozzleJournal of the Aerospace Sciences, 1959