Information from current and projected man bearing vehicles is used to estimate parameters such as size of cabin, number of crew, duration of flight, and possible heat loads for all stages of such journey; environmental requirements; main part of paper describes environmental engineering systems for small Earth-to-orbit vehicle, large space station, and lunar suit; possible emergencies and their countermeasures.
High altitude chambers and pressure suits and their part in manned flight to moon
Brit Interplanetary Soc -- J
British Interplanetary Society -- Journal ; 17 , n 8
1960
38 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
NTIS | 1974
|