Development and Testing of a Vortex-Driven, High-Regression Rate Hybrid Rocket Engine
34th, Joint propulsion conference ; 1998 ; Cleveland; OH
1998-01-01
ALL
Nos 98-3100 to 98-3883 with gaps
Conference paper
English
AIAA , ASME , SAE , ASEE , propulsion
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Persistent vortex generating high regression rate solid fuel grain for a hybrid rocket engine
European Patent Office | 2019
|Persistent vortex generating high regression rate solid fuel grain for a hybrid rocket engine
European Patent Office | 2024
|European Patent Office | 2022
|