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abstractrocket science has progressed greatly from its early development in the 1200’s. our research consists ofthe design, fabrication, launch, and recovery of a supersonic experimental sounding rocket with a target apogee of25,000 feet above ground level. the configuration of the rocket will consist of a booster stage with a second stage,designed to carry a ten pound payload. research has been conducted to mitigate trajectory failures, preventstructural damage, and locate the system after impact using beeline gps. an onboard data acquisition computerwill acquire data including; altitude, velocity, acceleration, and other important statistics. data measured will beused to validate computational models that are designed to predict the rocket’s trajectory. these models are based onnewton’s laws in two dimensions which include velocity, mass, and altitude as a function of time. a test rocket hasbeen used to begin the validation of the computational programs and to also verify design specifications of the finalrocket.
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