Braking arrangement for a spin-stabilized projectile

Details Braking arrangement for a spin-stabilized projectile Braking arrangement for a spin-stabilized projectile

1987-02-19

1988-02-23

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Remote control

102386, F42B 1502

Patent

active

047265434

ABSTRACT:
A braking arrangement for a spin-stabilized projectile, which provides for an increase in the effective surface on the projectile which is contacted by onflowing air, and which is activated in dependence upon the time of flight. There is provided a braking sail which is radially outwardly stretchable or expandable by means of centrifugal masses or flyweights.

REFERENCES:
patent: 3047259 (1963-07-01), Tatnall et al.

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