Turbojet afterburner engine with two-position exhaust nozzle

Details Turbojet afterburner engine with two-position exhaust nozzle Turbojet afterburner engine with two-position exhaust nozzle

1978-01-25

1981-01-06

Hart, Douglas

Power plants

Reaction motor

Condition responsive thrust varying means

60261, 60271, 23926515, F02K 124, F02K 310

Patent

active

042428653

ABSTRACT:
A turbojet afterburner engine has an expendable nozzle portion which can be jettisoned when the afterburner is placed in operation.

REFERENCES:
patent: 2766581 (1956-10-01), Welsh
patent: 2880576 (1959-04-01), Kappus
patent: 2910828 (1959-11-01), Meyer et al.
patent: 3011309 (1961-12-01), Carter
patent: 3030769 (1962-04-01), Badders
patent: 3171248 (1965-03-01), Ledwith
patent: 3331204 (1967-07-01), Love
patent: 3386248 (1968-06-01), Pike et al.

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