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.


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    Mars Penetrator Telemetry and Control System

    R. D. Bentley / A. B. Campbell | NTIS | 1975


    Mars Sample Thermal Control During Mars Ascent and Orbit

    Bhandari, Pradeep / Redmond, Matt / Kempenaar, Jason | NTRS | 2016



    Mars Sample Thermal Control During Mars Ascent and Orbit

    Bhandari, Pradeep / Redmond, Matt / Kempenaar, Jason | NTRS | 2016