STUDY ON THE THERMAL DECOMPOSITION CHARACTERISTICS OF AP/HTPB COMPOSITE PROPELLANT UNDER HIGH HEAT FLUX (AIAA 2016-5119)
Joint propulsion conference
01.01.2016
11 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Thermal Decomposition of Composite HMX/HTPB Propellant
British Library Conference Proceedings | 1999
|DataCite | 1943
INTELLIGENT APPROACH FOR COLLABORATIVE SPACE ROBOT SYSTEMS (AIAA 2018-5119)
British Library Conference Proceedings | 2018
|AIAA | 1981
|