Accession Number : AD0857235
Title : Multiple Artillery Rocket System (MARS) Conceptual Design Studies. Appendix C. Engineering Drawings and Data. Part Two. Engineering Data.
Descriptive Note : Final study rept.
Corporate Author : NORTHROP CORP HUNTSVILLE AL
Report Date : JUL 1969
Pagination or Media Count : 289
Abstract : The following listed engineering data is contained in this part of Appendix C as reference and supporting study information for the MARS Final Study Report: Blast Loads and Heating Effect on Launcher Vehicle--Aerodynamic Heating Effect on Missile; Elastic Body Response of MARS Self-Propelled Launcher; Rigid Body Response; Power and Servo System for MARS Missile Launcher; and Structural Design Calculations.
Descriptors : *ARTILLERY ROCKETS, *ROCKET LAUNCHERS, ROCKET WARHEADS, BLAST, LOADS(FORCES), HEATING, HEAT TRANSFER, SERVOMECHANISMS, PITCH(MOTION), YAW, TOWED VEHICLES, SELF PROPELLED GUNS, AERODYNAMIC HEATING, STRUCTURAL PROPERTIES, THERMAL PROPERTIES, MATHEMATICAL MODELS.
Subject Categories : Rockets
Distribution Statement : APPROVED FOR PUBLIC RELEASE