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):
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:
Subject Categories:
- Fluidics and Fluerics
- Rockets