The analysis, design, test, and application of a first stage deceleration and stabilization balloon system (Ballute) for recovery of payloads up to Mach 10 between altitudes of 120,000-200,000 ft down to Mach 4 at 70,000 ft are discussed. Techniques of analysis, construction, deployment, and inflation are described; also, the developments of high-temperature materials, fabrication techniques, and results of wind tunnel, functional, environmental, and missile tests.Tests substantiate the feasibility of expandable structures for positive deceleration and stabilization. The Ballute system provides deceleration and stabilization at speeds and altitudes that are beyond the capabilities of present parachute systems. Its practicality has been established on the basis of reliability, minimum weight and bulk, standard manufacturing techniques, and availability of materials that can withstand high-load levels and high temperatures.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Expandable Balloon-Type Drag Devices for Mach 10 Flight Regime


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Nebiker, F. R. (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    1963-01-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Expandable balloon-type drag devices for mach 10 flight regime

    Nebiker, F.R. | Engineering Index Backfile | 1963


    Flight techniques for determining airplane drag at high Mach numbers

    Beeler, De E / Bellman, Donald R / Saltzman, Edwin J | NTRS | 1956


    Determination of balloon drag

    CONRAD, GEORGE / ROBBINS, EDWARD | AIAA | 1991


    Determination of balloon drag

    Conrad, George R. / Robbins, Edward J. | NTRS | 1991


    Drag and Total Pressure Distributions in Scramjet Engines at Mach 8 Flight

    Tohru Mitani / Tetsuo Hiraiwa / Yuichi Tarukawa et al. | AIAA | 2002