Turbopump assembly for modern liquid propellant rocket engine is complete system in itself. It consists of many components, some of which are themselves subsystems. Monograph deals with turbopump as system, covering selection of proper system type for each application and integration of components into working system.
Design criteria monograph on turbopump systems
01.07.1975
Sonstige
Keine Angabe
Englisch
Design criteria monograph on turbopump gears
NTRS | 1975
Design criteria monograph on turbopump inducers
NTRS | 1972