Design problems compared with those of conventional air conditioning systems; rules on which designs are based, heating and cooling loads, and development of air and vapor cycle systems are outlined; missile and rocket conditioning systems in relation to mission to be accomplished, and problems involved in orbital and space flights also discussed.
Air conditioning as applied to aircraft, missiles and rockets
ASHRAE J
ASHRAE Journal ; 2 , n 3
1960
7 pages
Aufsatz (Zeitschrift)
Englisch
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