Accession Number : ADD006489

Title :   Aeroload Torque Simulator.

Descriptive Note : Patent Application,

Corporate Author : DEPARTMENT OF THE ARMY WASHINGTON DC

Personal Author(s) : Carter ,James W ; Lee ,Donald C ; Simeone ,Vincent A ; Cheever,Frank L

Report Date : 16 Apr 1979

Pagination or Media Count : 13

Abstract : The aeroload torque simulator provides torques for either statically or dynamically loading the output shaft of a power servo system such as a missile fin control system. It simulates the aerodynamic torque load developed at the missile fin which varies dynamically in flight. (Author)

Descriptors :   *Patent applications, *Guided missile simulators, *Fins, *Drive shafts, *Aerodynamic loading, *Torque, Servomechanisms, Flight control systems, Guided missile components, Servovalves

Subject Categories : Guided Missiles
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE