Missile fin unfolding device

Details Missile fin unfolding device Missile fin unfolding device

1988-02-08

1989-05-02

Basinger, Sherman D.

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

2441181, 2441374, 244 327, B64C 356

Patent

active

048261050

ABSTRACT:
A control surface deployment mechanism allows reliable, controlled launch of guided missiles from internal bays of high performance aircraft.

REFERENCES:
patent: 2876677 (1959-03-01), Clark et al.
patent: 3063375 (1962-11-01), Hawley et al.
patent: 4441674 (1984-04-01), Holtrop
patent: 4568044 (1986-02-01), DiTommaso et al.
patent: 4667899 (1987-05-01), Wedertz
patent: 4781342 (1988-11-01), Hardy et al.

Affiliated with

Also associated with

Rating

Missile fin unfolding device does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Missile fin unfolding device, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Missile fin unfolding device will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-579555