Ammunition and explosives – Igniting devices and systems
Patent
1975-11-05
1979-02-06
Pendegrass, Verlin R.
Ammunition and explosives
Igniting devices and systems
F42B 1500, F42B 1520
Patent
active
041378482
ABSTRACT:
An engine mount to position a rocket engine within a missile stage and to lease the engine upon burn-out. A separation ring comprising a bracket portion and a shroud portion encircles the engine. The bracket is located approximately mid-length of the engine and wound thereon to engage the engine-circling sheath having a grooved and unsymmetrically weakened cross-section. The shroud is joined to the interior of an on-flying missile stage. A small rocket and fail-safe abutment ensure that the motor will be released in a direction opposite to the continuing flight path of the parent stage.
REFERENCES:
patent: 3260204 (1966-07-01), Wilkey, Jr.
patent: 3453960 (1969-07-01), Qualls
patent: 3486410 (1969-12-01), Drexelius
patent: 3534686 (1970-11-01), Watson
Curry Charles D. B.
Gray Francis I.
Pendegrass Verlin R.
Sciascia R. S.
The United States of America as represented by the Secretary of
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