Investigation of Regression Rate under High-Pressure in Axial-Injection End-Burning Hybrid Rockets (AIAA 2018-4529)
Joint propulsion conference
01.01.2018
10 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2017
|British Library Conference Proceedings | 2016
|