Non-continuous ignition train

Details Non-continuous ignition train Non-continuous ignition train

1982-12-03

1991-07-30

Bentley, Stephen C.

Power plants

Combustion products used as motive fluid

Combustion products generator

60245, 60256, F02K 718, F02K 995

Patent

active

050351125

ABSTRACT:
A pyrotechnic ignition train for use in dual nozzle rocket-ramjet missiles herein a donor device and a receptor charge in the train allow transfer of a pyrotechnic impulse across an air gap between an outer nozzle and an inner concentric nozzle to allow ignition of the rocket motor. Upon consumption of the rocket fuel the inner nozzle is jettisoned, and the ramjet motor fired. Absence of physical connection of the nozzles at the ignition train allows easy separation of the inner nozzle from the missile.

REFERENCES:
patent: 2976680 (1961-03-01), Kobbeman
patent: 2987875 (1961-06-01), Fox
patent: 3000306 (1961-09-01), Wenzel et al.
patent: 3084504 (1963-04-01), McKinnon
patent: 3173252 (1965-03-01), Ziegenhagen
patent: 3273335 (1966-09-01), Gravlin et al.
patent: 3529418 (1970-09-01), Puckett et al.
patent: 3547031 (1970-12-01), Black et al.
patent: 3855789 (1974-12-01), Platzek

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