Results 21 to 30 of about 49,027 (122)
This investigation was devoted to exploring the thermal decomposition and sensitivity characteristics of solid propellants using nano-AN and nano-AP as oxidizers.
Xiaolan Song +6 more
doaj +1 more source
This work deals with energy performance calculate results of new solid composite propellants based on Hexanitroethane (HNE) and Hydrazinium nitroformate (HNF).
Li-nan Zhang +5 more
doaj +1 more source
ReaxFF molecular dynamics simulations on thermal decomposition of RDX-based CMDB propellants
Abstract ReaxFF molecular dynamics (ReaxFF MD) simulations were performed to study the thermal decomposition property of cyclotrimethylenetrinitramine (RDX) based composite modified double base (CMDB) propellants. The intermediate products and final products of the decomposition of RDX based CMDB propellants at 2000 K, 2500 K and 3000 K are ...
Huanan, Wei +3 more
openaire +2 more sources
Different models were provided to predict the storage lifetime of propellants more accurately. The stabilizer was recognized as a vital parameter for double based propellants’ storage lifetime estimation.
Qiong Wang +4 more
semanticscholar +1 more source
Optical Diagnostics for Solid Rocket Plumes Characterization: A Review [PDF]
In recent decades, solid fuel combustion propulsion of spacecraft has become one of the most popular choices for rocket propulsion systems. The reasons for this success are a wide range of applications, lower production costs, simplicity, and safety. The
De Giorgi M. G. +3 more
core +2 more sources
Molecular Dynamics of Neutral Polymer Bonding Agent (NPBA) as Revealed by Solid-State NMR Spectroscopy [PDF]
Neutral polymer bonding agent (NPBA) is one of the most promising polymeric materials, widely used in nitrate ester plasticized polyether (NEPE) propellant as bonding agent.
Cai, Rulin +6 more
core +1 more source
The combustion efficiency of HMX-CMDB propellants.
The effects of addition of nitramine compound to a double-base propellant on the combustion efficiency were investigated. HMX was used as a nitramine compound. Reaction time in the dark zone, heat of explosion, and gaseous combustion products were measured.
Yutaka YANO, Tsutomu GOMI
openaire +2 more sources
Nitramine Double Base Propellants [PDF]
This review paper broadly covers the studies conducted on nitramine double base (DB) propellants, particularly in the field of formulations, evaluation, catalysis and combustion mechanism .
Bhalerao, M. M. +3 more
core +2 more sources
Effects of carbon dots and their composites on the burning performance of HMX-CMDB propellant
Zhen Zhang +11 more
openaire +2 more sources
Cross-Linked Slurry Cast Composite Modified Double Base Propellants : Mechanical Properties [PDF]
Cross-linking of NC by TDI in slurry cast CMDB propellant enhanced TS by about 100 per cent. Coated AP with resorcinol, phloroglucinol, hexanetriol or silicone oil etc. along with cross-linking of NC raised TS from 18 - 30 kg/cm2.
Bhat, V. K., Singh, Haridwar
core +2 more sources

