Evolution of attitude control systems related to NASA space vehicles is covered; successful employment of electric thrust vector control on Mercury-Redstone was followed by employment of fluid power for Juno II, Saturn, and advanced Saturn; comparison made of electric and hydraulic systems as exemplified by Pershing and Mercury-Redstone; other applications of fluid power related to space vehicles; advantages of fluid power.
Technical advantages of fluid power
SAE -- Paper
SAE Meeting ; 1962 Hydraulic equipment
1962
39 pages
Aufsatz (Konferenz)
Englisch
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