Solid propellant vehicle to perform probe, re-entry, and orbital research missions may be ground launched or given initial boost by first stage using fin configuration to provide stability; tests to determine effects of fin area, antennas and wiring tunnels on stability at Mach 2.29, 2.96, 3.96, and 4.65 and Re of 3.5×106/ft.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Investigation of static longitudinal and lateral stability characteristics of 0.10-scale model of three-stage configuration of scout research vehicle at Mach numbers of 2.29, 2.96, 3.96, and 4.65


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English