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.
MARS II Control System
1968
13 pages
Report
Keine Angabe
Englisch
Hydraulic & Pneumatic Equipment , Rockets , Artillery rockets , Gas generating systems , Flight control systems , Performance(Engineering) , Pneumatic valves , Check valves , Fluid amplifiers , Exhaust nozzles , Mechanical drawings , Assembly , Fluerics , Mars(Multiple artillery rocket system) , Mars-2 missiles , Multiple operation
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