Design and Analysis of a Reusable N2O-Cooled Aerospike Nozzle for Labscale Hybrid Rocket Motor Testing
Author(s) -
Daniel Joseph Grieb,
Patrick Lemieux,
W. J. Murray,
Joseph Mello,
T. E. Cooke,
James Gerhardt
Publication year - 2011
Publication title -
digitalcommons (california polytechnic state university)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2011-5539
Subject(s) - nozzle , aerospace engineering , rocket (weapon) , solid fuel rocket , rocket engine , materials science , automotive engineering , mechanical engineering , propellant , aeronautics , computer science , engineering
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