Aerodynamic heating environment definition/thermal protection systemselection for the HL-20
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25565
Reference30 articles.
1. 21st century space transportation system design approach - HL-20 personnel launch system
2. Aerodynamic characteristics of the HL-20
3. Ascent abort capability for the HL-20
4. HL-20 computational fluid dynamics analysis
5. Six-degree-of-freedom guidance and control-entry analysis of the HL-20
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