Rocket Propulsion Elements by Sutton George P. Biblarz Oscar & Oscar Biblarz

Rocket Propulsion Elements by Sutton George P. Biblarz Oscar & Oscar Biblarz

Author:Sutton, George P.,Biblarz, Oscar & Oscar Biblarz [Sutton, George P. & Biblarz, Oscar]
Language: eng
Format: epub
ISBN: 9781118753910
Publisher: John Wiley & Sons, Inc.
Published: 2016-11-07T00:00:00+00:00


Figure 10–2 Exploded view of an advanced high‐speed, two‐stage experimental liquid hydrogen fuel pump driven by a radial flow turbine.

Used with permission of Aerojet Rocketdyne. Adapted from Ref. 10–7.

Figure 10–3 Section view of early, typical geared turbopump assembly similar to the one used on the RS‐27 engine (Delta I and II launch vehicles) with liquid oxygen and RP‐1 propellants.

Courtesy of Aerojet Rocketdyne.

Figure 10–4 Simplified diagrams of several different component arrangements of turbopumps. F, fuel pump; O, oxidizer pump; T, turbine; G, hot gas; C, shaft coupling; and GC, gear case.

Used with permission from Ref. 10–1.



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