Cannon launched platform

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

74 51, 74 54, 74 56A, 75 57, F41G 700, G01C 1928, G01C 1912, G01C 1924

Patent

active

041555210

ABSTRACT:
A gyro seeker which is capable of use in a cannon launched missile. The gyro seeker is enclosed in a housing mounted in the nose section of the missile. The platform of the gyro seeker supports an optical assembly, a detector, a gyro assembly, and a cryostat for cooling the detector. Means are provided on the outer gimbal of the platform for withstanding the extreme acceleration induced by cannon launching. The platform is torqueable along two axes by a plurality of pole pieces located around its base. A platform caging device is provided to cage the platform during transport and serves a dual function as a means to furnish spin-up gas to the gyro element and cooling gas to the cryostat.

REFERENCES:
patent: 3187588 (1965-06-01), Parker
patent: 3446082 (1969-05-01), Speen et al.
patent: 3756538 (1973-09-01), McLean
patent: 3824865 (1974-07-01), Evans et al.
patent: 3920200 (1975-11-01), Evans et al.

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

Cannon launched platform does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFUS-PAI-O-1036792

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