Materials and structures for hypersonic vehicles
- 1 November 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 26 (11) , 953-970
- https://doi.org/10.2514/3.45868
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- Flow-thermal-structural study of aerodynamically heated leading edgesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Verification tests of durable thermal protection system conceptsJournal of Spacecraft and Rockets, 1985
- Introductory aerothermodynamics of advanced space transportation systemsJournal of Spacecraft and Rockets, 1985
- Honeycomb sandwich structure for future space transportation systemswith integral cryogenic tankageJournal of Spacecraft and Rockets, 1984
- Radiant heating tests of several liquid-metal heat-pipe sandwich panelsJournal of Spacecraft and Rockets, 1984
- Hydrocarbon rocket engines for earth-to-orbit vehiclesJournal of Spacecraft and Rockets, 1983
- Research in structures and materials for future space transportationsystems - An overviewJournal of Spacecraft and Rockets, 1983
- Structural Prospects for Hypersonic Air VehiclesAircraft Engineering and Aerospace Technology, 1966
- THERMANTIC STRUCTURE TEST PROGRAMPublished by Defense Technical Information Center (DTIC) ,1966
- DEVELOPMENT TEST SUMMARY IN SUPPORT OF X-20 ELEVON STRUCTURAL TEST PROGRAMPublished by Defense Technical Information Center (DTIC) ,1966