Accession Number : AD0851658

Title :   Post Flight Digital Simulation of the Atlas 40-D Missile,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Slaughter, J. B.

Report Date : 14 SEP 1960

Pagination or Media Count : 20

Abstract : The report contains the results of the post flight digital simulation of the Atlas XSM-65-40D missile. The missile was flight tested previously and the study was made by simulating the flight of the 40-D missile on the IBM 704 computer. (Author)

Descriptors :   (*SURFACE TO SURFACE MISSILES, FLIGHT TESTING), (*FLIGHT TESTING, DATA PROCESSING), COMPUTER PROGRAMMING, LIQUID PROPELLANT ROCKET ENGINES, WEIGHT, AERODYNAMIC CHARACTERISTICS, DRIFT, PROPELLANT CONTROL, CORRELATION TECHNIQUES.

Subject Categories : Surface-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE