Selection and design considerations of components for high performance turbopumps for aircraft or rocket engine applications; following conclusions reached: takeoff weight of rockets and missiles is directly effected by turbopump efficiency and required suction specific speed; turbine selection is governed by weight and efficiency; aircraft turbopumps are capable of operation at much higher speeds due to their shorter operating life. Bibliography.
High speed turbo pumps
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1956 Pumps
1956
59 pages
Aufsatz (Konferenz)
Englisch
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