Study on bullet impact performance of the HATO-based explosives [PDF]
In order to study the vulnerability of 1,1'-dihydroxy-5,5'-bistetrazole dihydroxylamine salt (HATO) based explosives, a comparative study of the bullet impact vulnerable characteristics of HATO-based explosives and HMX-based explosives were carried out ...
Gao, Zan +6 more
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Fabrication of CL-20/HMX Cocrystal@Melamine-Formaldehyde Resin Core-Shell Composites Featuring Enhanced Thermal and Safety Performance via In Situ Polymerization. [PDF]
Int J Mol Sci, 2022 Duan B +5 more
europepmc +1 more source
Manufacture and static firing of X259-E6 rocket motor serial number XJ04/0001 [PDF]
A single motor was cast and static fired to demonstrate the performance of high energy crosslinked double base (XLDB) propellant in standard X259 rocket motor hardware.
Robertson, D. R.
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Research Progress of Bonding Agents and Their Performance Evaluation Methods. [PDF]
Molecules, 2022 Gan J +7 more
europepmc +1 more source
Effect of Nano-Sized Energetic Materials (nEMs) on the Performance of Solid Propellants: A Review. [PDF]
Nanomaterials (Basel), 2021 Pang W +6 more
europepmc +1 more source
Examination of the small scale slow cookoff behavior of a cast modified double base propellant [PDF]
The slow cookoff behavior of a proprietary cast modified double base (CMDB) propellant was examined using a variety of diagnostic techniques with the ultimate goal of capturing aspects of the chemical, physical, and morphological behavior of the ...
Shen, Jeffrey D
core
Design of an aluminum powder combustor for simulating the combustion conditions in solid rocket motors [PDF]
, 1993 This research presents the design of a combustion device which will simulate the aspects of aluminum particle combustion inside a solid rocket motor. At the same time this combustor will allow optical data to be collected during the combustion process ...
Geierman, Robert John
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Performance, Stability and Erosivity of Nitrogen-Rich Gun Propellants [PDF]
, 2017 RÉSUMÉ Plusieurs chercheurs considèrent que les approches actuelles au contenu énergétique de propulsifs ont atteint leur maturité et leurs limites.
Lavoie, Jonathan
core
Burning rate characteristics of RDX-CMDB propellants.
Journal of the Japan Society for Aeronautical and Space Sciences, 1986 Yutaka YANO, Tsutomu GOMI
openaire +2 more sources
Dynamic Mechanical Response and Damage Mechanism of HTPB Propellant under Impact Loading. [PDF]
Materials (Basel), 2020 Zhang H +6 more
europepmc +1 more source