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A study of the application of microwave techniques to the measurement of solid propellant burning rates Progress report, 1 Sep. 1966 - 31 Aug. 1967 [PDF]
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Near-future rocket launches could slow ozone recovery. [PDF]
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Development of low cost ablative nozzles for solid propellant rocket motors, volume 1 Final report [PDF]
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Studies on the influence of testing parameters on dynamic and transient properties of composite solid rocket propellants using a dynamic mechanical analyzer [PDF]
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