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

Personal Author(s):

Report Date:

1969-07-01

Pagination or Media Count:

289.0

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