Potential Benefits of Pressure Gain Combustion in Liquid Rocket Engine Pre-Burners (AIAA 2015-3762)
Joint propulsion conference
2015-01-01
11 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
DataCite | 1917
Fuel-rich Combustion Characteristics of Hybrid Rocket Engine (AIAA 2015-3828)
British Library Conference Proceedings | 2015
|British Library Conference Proceedings | 2018
|British Library Conference Proceedings | 2015
|