This study investigates and evaluates Mini-RPV launch concepts potentially suitable for the U. S. Army tactical environment. The air vehicle on which the launch study is based is the U. S. Army/Lockheed Aquila XMQM-105 Mini-RPV at a nominal gross weight of 120 pounds. A hypothetical RPV counterpart at 200 pounds gross weight is also used to bound the upper weight limit for Mini-RPVs. As a result of the Mini-RPV concept investigations and evaluations, it is recommended that in-depth studies be initiated to provide information for higher level evaluations based on detailed technical definitions related to both the pneumatic and the rocket-boosted systems. Additionally, information on the effects of parachute recovery on RPV and launcher design parameters is provided.


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    Titel :

    Mini-RPV Launch System Conceptual Study


    Beteiligte:
    H. E. Dickard (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    216 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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