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  1. 1
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    Performance of a towed, 48-inch-diameter (121.92-cm) ballute decelerator tested in free flight at Mach numbers from 4.2 to 0.4 / by Usry, J. W.

    Published 1969
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    Government Document eBook

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  2. 2
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    Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas / by Bahrami, Parviz A. (Parviz Ahmadi)

    Published 2012
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    Online Access
    Government Document eBook

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