Effects of environmental and ablator performance uncertainties on heat-shielding requirements for hyperbolic entry vehicles.
1968; American Institute of Aeronautics and Astronautics; Volume: 5; Issue: 11 Linguagem: Inglês
10.2514/3.29467
ISSN1533-6794
AutoresW. D. Coleman, L. F. HEARNE, J. M. Lefferdo, Liam Gallagher, N. S. Vojvodich,
Tópico(s)Gas Dynamics and Kinetic Theory
ResumoCovers advancements in spacecraft and tactical and strategic missile systems, including subsystem design and application, mission design and analysis, materials and structures, developments in space sciences, space processing and manufacturing, space operations, and applications of space technologies to other fields.
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