Accession Number:

AD0871333

Title:

MARS II Control System,

Descriptive Note:

Corporate Author:

ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL GUI DANCE AND CONTROL DIRECTORATE

Personal Author(s):

• Hodges, William H.

Report Date:

1968-09-01

Pagination or Media Count:

13.0

Abstract:

The report describes efforts to design and fabricate a hybrid pneumatic control system for the 16-inch diameter MARS II missile, with all components mounted at the rear on the missile nozzle, with a view to utmost simplicity in package assembly, quick interchange of parts, elimination of tubing and plumbing insofar as possible, and to present a neat and compact package.

Descriptors:

• *ARTILLERY ROCKETS
• *GAS GENERATING SYSTEMS
• FLIGHT CONTROL SYSTEMS
• PERFORMANCE(ENGINEERING)
• PNEUMATIC VALVES
• CHECK VALVES
• FLUID AMPLIFIERS
• EXHAUST NOZZLES
• ENGINEERING DRAWINGS
• ASSEMBLY

Subject Categories:

• Fluidics and Fluerics
• Rockets

Distribution Statement:

APPROVED FOR PUBLIC RELEASE