21st century space transportation system design approach - HL-20 personnel launch system
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/10.2514/3.25561
Reference20 articles.
1. Ascent abort capability for the HL-20
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1. Assessment of an Inviscid Euler-Adjoint Solver for Prediction of Aerodynamic Characteristics of the NASA HL-20 Lifting Body;34th AIAA Applied Aerodynamics Conference;2016-06-10
2. Feasibility of Guided Entry for a Crewed Lifting Body Without Angle-of-Attack Control;Journal of Guidance, Control, and Dynamics;2014-05
3. Variable Angle-of-attack Profile Entry Guidance for a Crewed Lifting Body;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05
4. Advanced TSTO Vessel Design for Safe and Inexpensive Human Orbital Access;AIAA SPACE 2008 Conference & Exposition;2008-06-15
5. Aerospace Vehicle Trajectory Design and Optimization Within a Multi-Disciplinary Environment;Journal of Aerospace Computing, Information, and Communication;2006-09
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