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:

1969-06-25

Pagination or Media Count:

106.0

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