Accession Number : AD0747841

Title :   Aerodynamic and Flight Simulation Study II. Volume I.

Descriptive Note : Technical rept.,

Corporate Author : CHRYSLER CORP HUNTSVILLE ALA HUNTSVILLE SPACE OPERATIONS

Personal Author(s) : Lindle,Charles A. , Jr

Report Date : 25 JUN 1969

Pagination or Media Count : 106

Abstract : The report presents the results of a study to perform a technical evaluation of the accuracy of certain foreign antiarmor missiles. A flight simulation computer program is described. Input data used in the flight simulator and the accuracy of specific missiles are presented. (Author)

Descriptors :   (*ANTIARMOR AMMUNITION, AERODYNAMIC CHARACTERISTICS), GUIDED MISSILES, ANGLE OF ATTACK, PITCH(MOTION), YAW, ROLL, AERODYNAMIC CONTROL SURFACES, GUIDANCE, COMPUTER PROGRAMS

Subject Categories : Guided Missiles
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE