Efforts made in lifting re-entry design and area of reusability; desirable aerodynamic characteristics of lifting re-entry vehicle for each speed regime in which flight will be conducted and advanced design profiles; examination of hypersonic drag polar; possible approaches by means of thermally shielded hot structure, uncooled thick-skinned hot structure, or cooled structure; molybdenum and columbium developments. (p 40-42 + 76 + 78 + 80 + 82 + 84)
Drive for lifting re-entry vehicles
Astronautics
Astronautics ; 6 , n 8
1961
Article (Journal)
English
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