2013-2014 Project Nova. Critical Design Review Presentation. Final Launch Vehicle Dimensions. Final Launch Vehicle Dimensions. Nosecone. Final Launch Vehicle Dimensions. Recovery Section. Final Launch Vehicle Dimensions. Booster Section. Final Launch Vehicle Dimensions.
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Critical Design Review Presentation
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Wildman Rocketry (Van Orin, IL)
Optimum Weight: 68.5 lbm
Mass margin: 22%
Apogee Achieved (ft): 15,508
Maximum Mach #: 1.02
Stability caliber: 2.93
Subscale Fin Dimensions