Results 1 to 10 of about 49,027 (122)
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 +5 more sources
Composite modified double base (CMDB) propellants are heterogeneous propellants in which properties are significantly improved by adding solid particles into the polymer matrix.
Kan Xie +6 more
doaj +3 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 +3 more sources
The effect of strain rate on compressive behavior and failure mechanism of CMDB propellant
The compressive mechanical behavior of composite modified double base (CMDB) propellant was investigated across a wide scope of strain rates ranging from 10−3 s−1 to 4210 s−1 at room temperature, by applying a conventional universal testing machine and a
Heng-ning Zhang +4 more
doaj +3 more sources
Mechanical Behaviors and Constitutive Relations under wide strain rate range for CMDB propellant
Propellant materials are occasionally experiencing severe dynamic loading during transporting and service process, thus their mechanical characteristics and potential mechanisms under transient loading are needed thoroughly understanding for its ...
Meng Li +4 more
doaj +3 more sources
In this study, the effect of the axial gap on the mechanical response of a cartridge-loaded propellant grain under vibration loads is investigated. The wide strain rate range of uniaxial compression tests (1.7×10−3~4×103 s−1) on the composite modified ...
Yiming Zhang +6 more
doaj +2 more sources
Combustion process of a promising catalyst [Cu(Salen)] for HMX-CMDB propellants. [PDF]
Metal organic complexes are regarded as a series of promising combustion catalysts for solid rocket propellants.
Ma W, Yang Y, Jia Y, Fu D, Zhao F, Xu K.
europepmc +3 more sources
Effect of Metal Nanopowders on the Performance of Solid Rocket Propellants: A Review [PDF]
The effects of different types of nano-sized metal particles, such as aluminum (nAl), zirconium (nZr), titanium (nTi), and nickel (nNi), on the properties of a variety of solid rocket propellants (composite, fuel-rich, and composite modified double base (
Weiqiang Pang +7 more
doaj +2 more sources
The frequent occurrence of safety accidents during the calendering process is caused by the flammable and explosive properties of composite modified double-base (CMDB) propellant.
Su-wei Wang +8 more
doaj +2 more sources
Simplified Burn-Rate Model for CMDB Propellants [PDF]
A single model has been proposed to predict the burning rates of bimodal AP,RDX and aluminum containing CMDB propellants. This is done in terms of the respective physical constants on the basis of a recently developed model of combustion of CMDB propellants.
A. R. Kulkarni +3 more
openaire +3 more sources

