Ascent abort capability for the HL-20
- 1 September 1993
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 30 (5) , 628-634
- https://doi.org/10.2514/3.25575
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
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- Aerodynamic characteristics of the HL-20Journal of Spacecraft and Rockets, 1993
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- 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
- Human factors evaluation of the HL-20 full-scale modelJournal of Spacecraft and Rockets, 1993