Conceptual design of a fully reusable manned launch system
- 1 July 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 29 (4), 529-537
- https://doi.org/10.2514/3.25496
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Design options for advanced manned launch systems (AMLS)Published by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Propulsion system optimization for Advanced Manned Launch System vehiclesJournal of Spacecraft and Rockets, 1990
- Aerodynamic separation and glideback of a Mach 3 staged boosterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- SSME evolution for next generation launch systemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Propulsion evaluation for orbit-on-demand vehiclesJournal of Spacecraft and Rockets, 1986
- Verification tests of durable thermal protection system conceptsJournal of Spacecraft and Rockets, 1985