Aeronautics and astronautics – Missile stabilization or trajectory control – Stabilized by rotation
Patent
1980-05-27
1982-09-21
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Stabilized by rotation
244 31, F42B 1332
Patent
active
043503152
ABSTRACT:
A method and apparatus are disclosed which are particularly adapted to quickly de-spin a rapidly rotating object or projectile. Weights are released from the object in a series of distinct stages, thus discarding enough momentum to reduce the spin of the object to a desired minimal value. The weights are released simultaneously by a single release means thereby assuring perfectly symmetrical and synchronized release of the respective weights. The result is a pure de-spin of the object without imparting other motion to the object.
REFERENCES:
patent: 2372383 (1945-03-01), Lee
Fedor, J. V. "Theory and Design Curves for a Yo-Yo De-Spin Mechanism for ellites," Aug. 1961.
Cornille, Jr.; Henry J., "A Method of Accurately Reducing The Spin Rate of a Rotating Spacecraft,"Oct. 1962.
Edelberg Nathan
Elbaum Saul
Gibson Robert P.
Jordan Charles T.
The United Staates of America as represented by the Secretary of
LandOfFree
Device to de-spin objects with very high spin does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Device to de-spin objects with very high spin, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Device to de-spin objects with very high spin will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-2072869