HL-20 concept - Design rationale and approach
- 1 September 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 30 (5) , 573-581
- https://doi.org/10.2514/3.25568
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Preliminary structural evaluation and design of the HL-20Journal of Spacecraft and Rockets, 1993
- Aerodynamic heating environment definition/thermal protection systemselection for 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
- Human factors evaluation of the HL-20 full-scale modelJournal of Spacecraft and Rockets, 1993
- HL-20 operations and support requirements for the Personnel Launch System missionJournal of Spacecraft and Rockets, 1993
- HL-20 subsystem designJournal of Spacecraft and Rockets, 1993