Rocket engine expansion nozzle with complementary annular nozzle

Power plants – Reaction motor – Plural motive fluid generating means or plural outlets

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60271, 23926523, 2394245, F02K 1100, B63H 2546

Patent

active

050673165

ABSTRACT:
The invention comprises an expansion nozzle for a rocket engine destined to function successively in atmospheric and space conditions. The nozzle is comprised of a main wall defining a surface of revolution that splays outwardly and further comprises a complementary annular convergent divergent nozzle having an exhaust port and also having its axis coinciding with the principal axis of the main wall. The complementary annular nozzle is located outside the main wall and has a gas distribution torus cooperating with gas flow supply means to produce an annular flow of gas surrounding a main flow of gas exhausted at the down stream extremity of said main wall of the expansion nozzle. The annular flow of gas forms a source of static pressure P.sub.s that is substantially lower than atmospheric pressure P.sub.a. P.sub.s has a value of between 0.3 and 0.8 times P.sub.a.

REFERENCES:
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patent: 3013384 (1961-12-01), Smith
patent: 3121457 (1964-02-01), Whipple
patent: 4004416 (1977-01-01), Amelio
patent: 4242865 (1981-01-01), Harrison
patent: 4489889 (1984-12-01), Inman
patent: 4592509 (1986-06-01), Moss
patent: 4947644 (1990-08-01), Hermant

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