Modification of NASA Langley 8 Foot High Temperature Tunnel to provide a unique national research facility for hypersonic air-breathing propulsion systems
- 5 March 1984
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Computing pressure cure viscoelastic effects in solid propellants.Journal of Spacecraft and Rockets, 1972
- Methane-Air Combustion Gases as an Aerodynamic Test MediumJournal of Spacecraft and Rockets, 1972