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  1. 1
    RECONSTRUCTION OF ATTENUATED HYBRID MOTOR CHAMBER PRESSURE SIGNALS USING MAXIMUM LIKELIHOOD ESTIMATION AND OPTIMAL DECONVOLUTION
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  2. 2
    THRUST AUGMENTATION OF AN ADDITIVELY MANUFACTURED HYBRID ROCKET SYSTEM USING SECONDARY H2O2 INJECTION
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  3. 3
    MEDICAL GRADE N20/02 MIXTURES AS INEXPENSIVE AND VOLUMETRICALLY EFFICIENT OXIDIZERS FOR SMALL SPACECRAFT HYBRID PROPULSION SYSTEMS
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