Artigo Revisado por pares

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

ISSN

1533-6794

Autores

W. D. Coleman, L. F. HEARNE, J. M. Lefferdo, Liam Gallagher, N. S. Vojvodich,

Tópico(s)

Gas Dynamics and Kinetic Theory

Resumo

Covers 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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