Missile with highly backswept wing unit, in particular with delt

Details Missile with highly backswept wing unit, in particular with delt Missile with highly backswept wing unit, in particular with delt

1983-10-25

1986-07-22

Tudor, Harold J.

Aeronautics and astronautics

Missile stabilization or trajectory control

Externally mounted stabilizing appendage

244 49, F42B 1502

Patent

active

046014420

ABSTRACT:
Unmanned missile with strongly backswept wing unit, in particular delta wings, which is transported in a container and is launched from the container by means of an auxiliary drive after release of a lock, and which during cruise flight is drivable by a propeller engine, lateral force surfaces (25) being deployable for stabilization of the missile during cruise flight, from retraction spaces (26) in the region of the wing root of the delta wings, and further a friction clutch (64, 65) is provided at the missile which, without supply of energy from the outside, couples the standing propeller 6 with the drive motor (7) running in the container, after leaving the container.

REFERENCES:
patent: Re25418 (1963-07-01), Grant
patent: 3285542 (1966-11-01), Holmquist
patent: 4106727 (1978-08-01), Ortell
patent: 4247063 (1981-01-01), Jenkins
patent: 4296894 (1981-10-01), Schnabele et al.
patent: 4410151 (1983-10-01), Happner et al.

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