Missile rolling tail brake torque system

Details Missile rolling tail brake torque system Missile rolling tail brake torque system

1982-01-11

1984-01-17

Goldberg, Gerald

Measuring and testing

Frictional resistance, coefficient or characteristics

73167, 73432R, G01N 1902, G01M 1900

Patent

active

044257856

ABSTRACT:
Apparatus for simulating varying levels of friction in the bearings 13 of a free rolling tail afterbody 11 on a canard-controlled missile 12 to determine friction effects on aerodynamic control characteristics. A ring 16 located between the missile body and the afterbody is utilized in a servo system to create varying levels of friction between the missile body and the afterbody to simulate bearing friction.

REFERENCES:
patent: 4154489 (1979-05-01), Lyman
patent: 4169367 (1979-10-01), Wunder et al.
patent: 4235092 (1980-11-01), Spall
patent: 4308490 (1981-12-01), Habermann et al.

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