21st century space transportation system design approach - HL-20 personnel launch system
- 1 September 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 30 (5) , 521-528
- https://doi.org/10.2514/3.25561
Abstract
No abstract availableKeywords
This publication has 14 references indexed in Scilit:
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- HL-20 computational fluid dynamics analysisJournal of Spacecraft and Rockets, 1993
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- Effect of lift-to-drag ratio in pilot rating of the HL-20 landing taskJournal of Spacecraft and Rockets, 1993
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- Aerodynamic characteristics of the HL-20Journal of Spacecraft and Rockets, 1993
- Ascent abort capability for the HL-20Journal of Spacecraft and Rockets, 1993
- Evaluation of the national launch system as a booster for the HL-20Journal of Spacecraft and Rockets, 1993
- Titan III feasibility for HL-20 prototype missionsJournal of Spacecraft and Rockets, 1993
- HL-20 operations and support requirements for the Personnel Launch System missionJournal of Spacecraft and Rockets, 1993