Multiple Artillery Rocket System (MARS) Conceptual Design Studies. Appendix C. Engineering Drawings and Data. Part Two. Engineering Data.

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.

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1969
Accession Number
AD0857235

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Heating
  • Artillery
  • Artillery Rockets
  • Blast Loads
  • Engineering
  • Engineering Drawings
  • Heating
  • Launchers
  • Rockets
  • Self Propelled
  • Vehicles
  • Weapons

Readers

  • Business Analytics
  • Military Science
  • Software Engineering