Dual expander rocket engine

Power plants – Reaction motor – Interrelated reaction motors

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60259, 60260, 60263, 60271, 23926527, F02K 906, F02K 902, B64C 1504

Patent

active

042200016

ABSTRACT:
A composite cycle rocket engine having an inner engine disposed to discharge directly into the nozzle of an outer engine, is described herein.

REFERENCES:
patent: 2408111 (1946-09-01), Truax et al.
patent: 2816417 (1957-12-01), Bloomberg
patent: 2981059 (1961-04-01), Horner et al.
patent: 3034293 (1962-05-01), Ferris et al.
patent: 3261571 (1966-07-01), Pinnes
patent: 3523422 (1970-11-01), Wolf
patent: 3541795 (1970-11-01), Nelson
patent: 3613375 (1971-10-01), Abild
patent: 3636712 (1972-01-01), Kaufmann
patent: 3871173 (1975-03-01), McKenna
patent: 3955784 (1976-05-01), Salkeld
Aviation Week & Space Technology, Sep. 19, 1966, pp. 60-61, 63, 65.

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