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.
Multiple Artillery Rocket System (MARS) Conceptual Design Studies. Appendix C. Engineering Drawings and Data. Part Two. Engineering Data
1969
289 pages
Report
Keine Angabe
Englisch
Rockets , Artillery rockets , Rocket launchers , Design , Data , 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 , Mars(Multiple artillery rocket systems) , Multiple operation
Dual Dimensioning Engineering Drawings
SAE Technical Papers | 1999
Rocket Artillery Launch Spotter (RLS)
NTIS | 2006
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