Quick conversion missile system for widebody aircraft

Ordnance – Rocket launching – Movable launcher

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

89 1801, F41F 306

Patent

active

044896387

ABSTRACT:
A missile launching system adapted for installation in a standard commercial aircraft without modification of the aircraft structure. The system comprises a plurality of frame members, linear tracks which are movable longitudinally relative to the frame members, a plurality of launch tubes for storing the missiles, an exit port for installation in an pre-established aircraft fuselage opening, and associated equipment for selectively launching the missiles from the launch tubes through the exit port. The entire system is assembled from individual components, all of which are sized to be placed on board the aircraft through a standard passenger door opening. In preparation for installing the system in a commercial aircraft, the passenger seats and related equipment conventionally installed in the interior of such an aircraft are removed. The frame members of the system are then mounted to the standard seat tracks in the floor of the aircraft. The remaining portions of the system are thereafter assembled and installed on the frame. The frame is inclined to support the launch tubes at an angle extending upward and forward so that when a missile is ejected from the launch tube, it is given a trajectory which carries it clear of the aircraft wing and empennage.

REFERENCES:
patent: 2566390 (1951-09-01), Weber
patent: 2709947 (1955-06-01), Woods
patent: 2731885 (1956-01-01), Nolan
patent: 2789470 (1957-04-01), Bronson
patent: 2803168 (1957-08-01), Robert et al.
patent: 2826120 (1958-03-01), Lang et al.
patent: 2845004 (1958-07-01), Johnson
patent: 2938434 (1960-05-01), Myron
patent: 2973691 (1961-03-01), Goldsmith
patent: 2989899 (1961-06-01), Siegel et al.
patent: 3534653 (1970-10-01), Specht et al.
patent: 3583277 (1971-06-01), Crockett
patent: 4012985 (1977-03-01), Magnusson
patent: 4040334 (1977-08-01), Smethers, Jr.
patent: 4106389 (1978-08-01), Walley
patent: 4208949 (1980-06-01), Boilsen
patent: 4256012 (1981-03-01), Cowart et al.
patent: 4318328 (1982-03-01), Rona
patent: 4333384 (1982-06-01), Arnold
patent: 4409880 (1983-10-01), Fetterly

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Quick conversion missile system for widebody aircraft does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Quick conversion missile system for widebody aircraft, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Quick conversion missile system for widebody aircraft will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1147377

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.