This contract covers the design, development, testing and delivery of an improved rocket for the flechette warhead. Work included (1) design, analysis, and component tests; (2) development tests; (3) Preliminary Flight Rating Tests; and (4) delivery of improved rocket motors. Analyses included design trade-off studies, aerodynamics analysis, and manufacturing optimization studies. The improved design was successfully demonstrated through the preliminary flight rating tests and through flight tests, both ground-launched and aircraft-launched. Performance, reliability, and accuracy are within contract requirements. This final report is in two volumes. Volume I contains the program accomplishments and Volume II (AD-501 433) contains the Appendixes. (Author)


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    2.75-In. Folding Fin Aircraft Rocket. Volume 2. Appendixes

    G. Dolgonas / H. A. Krayenbuhl | NTIS | 1969




    An Improved Canadian 2.75-Inch Rocket Motor

    F. Jackson / F. A. Christie / M. N. Clark et al. | NTIS | 1976


    Aerodynamic Properties of the 2.75-Inch Rocket T131

    L. C. MacAllister / W. K. Rogers | NTIS | 1955