Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1990-03-15
1991-05-07
Carone, Michael J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
F41G 732
Patent
active
050129910
ABSTRACT:
A tube-launched projectile includes an airframe with an open aft end, an optical fiber dispensing bobbin, and an obturator having a rocket motor attached to a hard point in the aft end of the airframe. The obturator forms a pressure vessel with insulated inner walls which contain rocket propellant and an igniter. An ejectable plug located in the rocket nozzle is expelled upon motor ignition.
REFERENCES:
patent: 3233548 (1966-02-01), Chilowsky
patent: 3673963 (1972-07-01), McGowan
patent: 3753537 (1973-08-01), Karpa et al.
patent: 3868883 (1975-03-01), Tucker
patent: 4770370 (1988-09-01), Pinson
patent: 4796833 (1989-01-01), Pinson
patent: 4860968 (1989-08-01), Pinson
patent: 4907763 (1990-03-01), Pinson
patent: 4967980 (1990-11-01), Pinson
Carone Michael J.
The Boeing Company
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