MARS II Control System,

reportActive / Technical Report | Accession Number: AD0871333 | Need Help?

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.

Author(s):
Hodges, William H.
Author Organization(s):
ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL GUI DANCE AND CONTROL DIRECTORATE
Pagination:
0013

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
RG-TM-68-2
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means
Communities of Interest:
Weapons Technologies
Descriptor(s):
*ARTILLERY ROCKETS, *GAS GENERATING SYSTEMS, FLIGHT CONTROL SYSTEMS, PERFORMANCE(ENGINEERING), PNEUMATIC VALVES, CHECK VALVES, FLUID AMPLIFIERS, EXHAUST NOZZLES, ENGINEERING DRAWINGS, ASSEMBLY
Field(s)/Group(s):
Fluidics and Fluerics, Rockets
Keyword(s):
FLUERICS, MARS(MULTIPLE ARTILLERY ROCKET SYSTEM), MARS 2 MISSILES, ARTILLERY ROCKETS, MULTIPLE OPERATION
Report Date:
1968 Sep 01