The Use of a 3-D Printed, Polymer Matrix Containing Pulverized Fuel in a Hybrid Rocket (AIAA 2018-4597)
Joint propulsion conference
01.01.2018
6 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
NUMERICAL METHOD TO ESTIMATE THERMAL CONDUCTIVITY OF A MODEL COMPOSITE PROPELLANT (AIAA 2016-4597)
British Library Conference Proceedings | 2016
|Characterization of PolyMethylMethAcrylate as a Fuel for Hybrid Rocket Motors (AIAA 2018-4530)
British Library Conference Proceedings | 2018
|Numerical Study of Fuel Regression in Hybrid Rocket Engine (AIAA 2018-4593)
British Library Conference Proceedings | 2018
|British Library Conference Proceedings | 2018
|