Multiple Artillery Rocket System (MARS) Conceptual Design Studies. Appendix C. Engineering Drawings and Data. Part Two. Engineering Data.
Final study rept.
NORTHROP CORP HUNTSVILLE AL
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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.