Development of a steady-state shape change ablation code for the design of outer planet probes
Author:
Affiliation:
1. General Electric Co., Re-Entry and Environmental Systems Div., Philadelphia, Pa.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1977-95
Reference25 articles.
1. Viscous-shock-layer solutions with radiation and ablation injection for Jovian entry
2. Chin, J. H. "Advanced Composites II (RESEP II)-Vol.II, Computer User's Manual,Predictionof the Response of Graphite Nosetips - Version 2,Lockheed Missiles and Space Co., Report SAMSOTR-70-16, September 1969.
3. Nicolet, W. E., Morse, H. L., Neuner, G. J., and Gomez, A. V. "Outer Planet Probe Entry Thermal Protection", Aerotherm Final Report 74-92, February10,1975.
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