NON-CONTINUOUS IGNITION TRAIN
Assignee
US Government
Filed as: UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY, THE
Filed
Dec 3, 1982
Granted
Jul 30, 1991
Location
SAN JOSE CA US
Abstract
A pyrotechnic ignition train for use in dual nozzle rocket-ramjet missilesherein 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.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Mar 30, 1984
Rescinded
Mar 29, 1991
Duration
7 years
Inventor
- 1JOHN M. MC GARRY
Record Details
- Patent number
- US 5035112
- Application
- 06446833
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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