Small-scale Gaseous Oxygen Hybrid Rocket Testing Facility Upgrades for Regression Rate and Combustion Efficiency Studies (AIAA 2018-4439)
Joint propulsion conference
2018-01-01
9 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2017
|DataCite | 1930
Hybrid rocket combustion regression rate model.
AIAA | 1966
|