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Solid fuel regression rate in hybrid rocket is a key design parameter. An intrusive measurement technique is applied to a paraffin based fuel and preliminary results are compared with data coming from a revisited ballistic reconstruction procedure.
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This page is a summary of: Reconstructed Ballistic Data Versus Wax Regression-Rate Intrusive Measurement in a Hybrid Rocket, Journal of Spacecraft and Rockets, November 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34695.
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