Subordinate-ammunition missile with extendable glide wings

Details Subordinate-ammunition missile with extendable glide wings Subordinate-ammunition missile with extendable glide wings

1988-08-11

1989-09-26

Kyle, Deborah L.

Aeronautics and astronautics

Missile stabilization or trajectory control

Externally mounted stabilizing appendage

102393, 244 49, F42B 1332, F42B 1350

Patent

active

048694410

ABSTRACT:
A flying body for subordinate-ammunition missile with extendable glide wings. The flying body or missile of the above-mentioned type has the wings pivotally retained in attachments which are arranged generally in parallel with the longitudinal axis of the missile on the casing of the fuselage of the missile, and which are equipped with longitudinal grooves each respectively stowing a retracted wing.

REFERENCES:
patent: 3507150 (1970-04-01), Stengel
patent: 3647163 (1972-03-01), Sweeney
patent: 4364531 (1982-12-01), Knoski
patent: 4440360 (1984-04-01), Hallstrom
patent: 4455943 (1984-06-01), Pinson
patent: 4522356 (1985-06-01), Lair et al.
patent: 4558645 (1985-12-01), Boeder et al.
patent: 4635881 (1987-01-01), Brieseck et al.
"Defense Electronics", Jun. 1984, p. 102.
"Aviation Week & Space Technology", Mar. 2, 1981, p. 51.

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