Aerodynamic characteristics of the HL-20
- 1 September 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 30 (5) , 529-536
- https://doi.org/10.2514/3.25562
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Effect of lift-to-drag ratio in pilot rating of the HL-20 landing taskJournal of Spacecraft and Rockets, 1993
- Six-degree-of-freedom guidance and control-entry analysis of the HL-20Journal of Spacecraft and Rockets, 1993
- 21st century space transportation system design approach - HL-20 personnel launch systemJournal of Spacecraft and Rockets, 1993
- Ascent abort capability for the HL-20Journal of Spacecraft and Rockets, 1993
- Aerodynamic characteristics of the HL-20 and HL-20A lifting-body configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Aerodynamic characteristics of proposed assured crew return capability (ACRC) configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989