Entry corridor, for vehicles with and without lift, is bounded by flight regimes of excessive deceleration and insufficient aerodynamic drag; thermochemical and rarefaction effects of flow field in vehicle's vicinity are discussed; calculation methods for pressure distribution; review of aerodynamic heating, and estimates of its order of magnitude; transfer of heat by convection and by radiation are treated and data on corresponding heat fluxes are given; transpiration cooling and ablation-type heat protection.
Aerodynamic problems of hypersonic flight of sounding rockets through planetary atmosphere
Die aerodynamischen Probleme des hypersionischen Fluges von Raumsonden durch planetarische Atmosphaeren
Raumfahrtforschung ; 9 , n 2
1965
10 pages
Article (Journal)
German
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Optimization of Hybrid Sounding Rockets for Hypersonic Testing
Online Contents | 2012
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