DESIGN OF A LAB-SCALE HYDROGEN PEROXIDE/HYDROXYL TERMINATED POLYBUTADIENE HYBRID ROCKET MOTOR
39th, Joint propulsion conference; 39th AIAA/ASME/SAE/ASEE joint propulsion conference ; 2003 ; Huntsville, AL
01.01.2003
4744 pages
Nos 2003-4404 to 2003-9731 with gaps
Aufsatz (Konferenz)
Englisch
AIAA , ASME , SAE , ASEE , propulsion , aeronautics , automotive engineers , mechanical engineers , joint propulsion
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Thrust Modulation in a Nitrous Oxide/Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor
British Library Conference Proceedings | 2006
|Deep Throttle of a Nitrous Oxide and Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor
Online Contents | 2014
|