Ejector motor braking system

Details Ejector motor braking system Ejector motor braking system

1972-08-09

1977-05-17

Tudor, Harold

Ammunition and explosives

Igniting devices and systems

89 1818, F42B 1510

Patent

active

040234967

ABSTRACT:
A two stage separable missile adapted to be expelled from a launch tube by separable ejector motor and propelled along its trajectory by a flight motor ignited after the missile leaves the launch tube. The first stage includes a warhead, flight rocket motor and foldable tail fins. The second stage mounts on the rear of the first stage and encloses the folded tail fins. The second stage includes an ejector rocket motor for ejecting the missile from its tube and a braking motor for separating the first and second stages and decelerating the second stage to a zero velocity by the time it has traveled the length of the launch tube.

REFERENCES:
patent: 2821924 (1958-02-01), Hansen et al.
patent: 2940391 (1960-06-01), Brandt
patent: 3216357 (1965-11-01), Mertens
patent: 3308759 (1967-03-01), Sorenson
patent: 3380382 (1968-04-01), Jablansky
patent: 3457861 (1969-07-01), Crockett
patent: 3491689 (1970-01-01), Francois

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