Investigation of Flame Structures of Double-Base Propellant and Modified Double-Base Propellant Containing Nitramine Using OH-PLIF and Kinetic Simulation [PDF]
The combustion behavior of various propellant samples, including double-base propellants, pressed nitramine powders, and modified double-base propellants containing nitramine, was examined using OH-PLIF technology.
Yiping Wang +6 more
doaj +4 more sources
Modeling fatigue damage evolution in CMDB propellant based on dynamic modulus [PDF]
This study systematically investigates the fatigue behavior of composite modified double-base propellant (CMDB) under strain-controlled cyclic loading across a range of temperatures.
Li Yao +4 more
doaj +2 more sources
Study on elongation master curve of thermal aging composite modified double base propellant [PDF]
In order to predict the maximum elongation of composite modified double base (CMDB) propellants under different aging time, temperature and strain rate, systematic uniaxial tensile characterization was performed across six controlled temperatures (233.15
Jian Zheng +8 more
doaj +2 more sources
Experimental and machine learning-driven assessment of IS 2062 steel under double-base propellant combustion conditions [PDF]
The degradation behavior of IS 2062 structural steel under extreme combustion conditions induced by double-base propellant exposure is crucial for aerospace and defense applications.This study addresses in understanding steel performance under high ...
Hari Singh +3 more
doaj +2 more sources
Research on the influence of loading rate on the dynamic initiation fracture toughness of CMDB propellant [PDF]
In the field of gun launched missile extended range rocket, the propellant grain in the rocket needs to withstand significant launch loads during their firing phase, and also bear the high pressure caused by ignition, and the impact of launch overloads ...
Jian Zheng +5 more
doaj +2 more sources
Dynamic mechanical analysis of double base rocket propellants [PDF]
The article presents dynamic mechanical analysis (DMA) for solid rocket propellants testing. Principles of operation and measured values are briefly described.
Marcin Cegła +3 more
doaj +2 more sources
Propellant Combustion Wave Studies by Embedded Thermocouple and Imaging Method at Ambient Pressure [PDF]
This paper discusses the method for propellant combustion studies with embedded thermocouple and imaging method at ambient pressure. In this study, three different propellant compositions are experimentally evaluated for surface temperature, flame zone ...
Rakesh Kumar Kalal +3 more
doaj +2 more sources
Analysis of Application of Plasma Ignition in Closed Vessel Tests
This paper presents the results of a comparative investigation into the effects of the ignition method on the ballistic properties of three types of propellants: a single-base propellant, a double-base propellant and a low vulnerability (LOVA) propellant,
Radosław Trębiński +3 more
doaj +1 more source
Ispitivanja uticaja srednjeg masenog udela azota u nitrocelulozii veličine čestica modifikatora na brzine sagorevanja dvobaznih raketnih goriva / Investigation of the influence of the mass average ratio of nitrogen in nitrocellulose and the particle size on burning rates of double base propellants [PDF]
Istraživana je katalitička aktivnost balističkih modifikatora: baznog olovo-stearata, kalcijum-karbonata, kobalt (IH)-oksida i čadi, za različite masene udele azota u nitrocelulozi, kao komponenti dvobaznog raketnog goriva, kao i uticaj veličine čestica ...
Panto Maslak , Lajoš Tot
doaj +1 more source
Comparative study on ignition delay time and burning rate of modified double-base propellant and fuel-rich propellant [PDF]
With the higher requirements of various tactical and technical indicators of the weapon systems, the current research on the ignition and combustion characteristics of different types of solid propellants is not comprehensive.
LIAN-BO LI +3 more
doaj +1 more source

