Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1985-08-26
1987-04-21
Kyle, Deborah L.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
244 49, F42B 15053
Patent
active
046590374
ABSTRACT:
The invention concerns a missile body having a first flight guide and stabilization means mounted on the missile body and a second guide and stabilization means mounted on the missile body in front of the first guide and stabilization means with respect to the direction of flight. The second guide and stabilization means comprise a plurality of wings which are folded inwardly (collapsed inwardly, pivoted inwardly) into the missile body when in their inoperative position. These wings can be pivoted or slid outwardly when in their operative position by means of a collapsed expandable body which is expanded by means of pressurized gas. The pressurized gas is stored in a pressurized gas cylinder mounted within the missile body. The expandable body expands in a radial direction and thereby exerts a force on the wings which causes them to either pivot about a rotatable axis or to move in a radial direction outwardly of the missile body.
REFERENCES:
patent: 3047257 (1962-07-01), Chester
patent: 3633846 (1972-01-01), Biggs, Jr.
patent: 4143838 (1979-03-01), Holladay
patent: 4203569 (1980-05-01), Marks
patent: 4334657 (1982-06-01), Mattson
patent: 4364531 (1987-12-01), Knoski
patent: 4478150 (1984-10-01), Sayler et al.
patent: 4586681 (1986-05-01), Wedertz et al.
Carone Michael J.
Kyle Deborah L.
Rheinmetall GmbH
LandOfFree
Wing deploying system comprising an airbag does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Wing deploying system comprising an airbag, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Wing deploying system comprising an airbag will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-746460