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