Results 21 to 30 of about 49,027 (122)

Thermolysis and sensitivities of solid propellants using characterized nano oxidizers involving energy performance evaluation

open access: yesFirePhysChem, 2022
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

Effect of hexanitroethane (HNE) and hydrazinium nitroformate (HNF) on energy characteristics of composite solid propellants

open access: yesFirePhysChem, 2021
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

open access: yesJournal of Molecular Modeling, 2022
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

The Prediction of CMDB Propellant lifetime Based on Arrhenius accelerated model, Berthelot’s equation and Multi-step Prout-Tompkins Model

open access: yesJournal of Physics: Conference Series, 2021
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]

open access: yes, 2022
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]

open access: yes, 2014
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.

open access: yesJournal of the Japan Society for Aeronautical and Space Sciences, 1985
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]

open access: yes, 2013
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

open access: yesDefence Technology
Zhen Zhang   +11 more
openaire   +2 more sources

Cross-Linked Slurry Cast Composite Modified Double Base Propellants : Mechanical Properties [PDF]

open access: yes, 2014
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

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