Air-turbo-rocket, or ducted fan rocket, and ducted rocket, first studied by Germans during War, exhibit propensities for ultra-high speed, ultra-high altitude propulsion; British NGTE engine consists of modified turbojet in which turbine is driven by exhaust products of rocket type propellant mixture; turbine power is essentially independent of altitude and not subject to normal turbine entry temperature limitations introduced by high flight Mach number.
High-performance hybrid powerplants
Aeroplane
Aeroplane ; 92 , n 2376
1957
4 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
SAE Technical Papers | 1949
|Online Contents | 1994
Powerplants for High Performance ASW Vehicles
SAE Technical Papers | 1962
|