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