Aerospace plane and engine

Power plants – Reaction motor – Interrelated reaction motors

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Details

602701, F02K 718

Patent

active

051917610

ABSTRACT:
An engine for an aerospace plane has an inlet in association with which a core member is provided to render the inlet annular. The inlet leads into a combustion chamber and an outlet. The core member houses a rocket engine which, in use, induces ambient air to flow into the inlet at low and even zero speed, thus allowing the combustion chamber and outlet to be operated as a ram jet engine at low and even zero speed. By way of development, the core member houses oxygen liquification means adapted to capture ambient air and to liquify and separate oxygen therefrom. The oxygen is used in the rocket engine and allows the mass of on-board oxygen at take-off to be reduced. This increases the potential payload.

REFERENCES:
patent: 3374631 (1968-03-01), Marks
patent: 3541957 (1970-06-01), Evans
patent: 3690102 (1972-09-01), DuPont
patent: 4644746 (1987-02-01), Hartman
patent: 4817892 (1989-04-01), Janeke
Science Year: The World Book Annual Science Supplement 1988--resume.
Wall St. Journal--Jun. 19, 1989--2 pgs. Article.
Newspaper (unidentifiable) found Jul. 26, 1988 Article.
The Daily News (Durban) Jun. 13, 1987 Article.
Capital--Jun. 1987--Article.
Business Day--Apr. 8. 1986--Article.
European News--Apr. 1986--Article.
Aviation Week and Space Technology Apr. 14, 1986 --Article.
Aviation Week and Space Tecnhology Aug. 11, 1986--Article.
Newsweek--Aug. 1, 1987--Article.
Technology Review--pp. 43-55--Article.

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