Propulsion Options for the Hypersonic Research Airplane
- 1 July 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 12 (7) , 611-616
- https://doi.org/10.2514/3.59842
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- The case for a high-speed research airplane - Results from an in-house studyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- A new test capability for propulsion system testingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Key technology for airbreathing hypersonic aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Studies of Engine-Airframe Integration on Hypersonic AircraftJournal of Aircraft, 1971