Summary of requirements to consider in study of return, re-entry and recovery; reference made to Douglas thick-wing planetary vehicle which provides means of reducing maximum heating rate and total heating by entering atmosphere with winged vehicle placed at high total angle of attack; re-entry fundamentals; balloons and gliders; other concepts such as use of magnetohydrodynamic principles for increasing re-entry drag.
To hit entry corridor -- Descending space vehicles should have variable drag
Missiles Rockets
Missiles and Rockets ; 8 , n 22
1961
2 pages
Aufsatz (Zeitschrift)
Englisch
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