Results 11 to 20 of about 7,425 (303)
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
Advances in Structural Reliability Analysis of Solid Propellant Grain: A Comprehensive Review [PDF]
Hongfu Qiang, Xueren Wang
exaly +2 more sources
Performance Analysis of the Solid Rocket Propulsion System Using Solid Modeling and Level Set Method [PDF]
The performance prediction and grain burn-back analysis of rocket motor are important steps in the designing of a solid propellant rocket motor. The grain burn-back analysis of the solid grain identifies the burning surface area at each burning step in ...
Kyung Moo Kim, Doo Hee Han, Min Kyum Kim
doaj +1 more source
Aiming at the structural response characteristics of solid rocket motor (SRM) under vertical storage conditions, the creep tests of HTPB propellant under different stress levels were carried out, and the creep constitutive model of the propellant was ...
CHEN Ke +4 more
doaj +1 more source
Methodology for Testing High-Energy Materials Under Low Temperature Conditions [PDF]
The methodology developed for testing gun propellants at low temperatures according to PN-EN ISO 604:2006 is presented in the paper. Brief characteristics are given of the materials tested and the most important static compression test conditions, such ...
Patryk MODRZEJEWSKI, Jacek JANISZEWSKI
doaj +1 more source
Self-assembly of self-propelled magnetic grains [PDF]
In this work, we study bidisperse mixtures of self-propelled magnetic particles of different shapes via discrete element method simulations. We show how these particles self-assemble into clusters and how these clusters depend on the ratio of the mixture, the magnetic interaction, and the shape of the grains.
Marcos A. Madrid +3 more
openaire +2 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 +1 more source
Using the Impulse Method to Determine High-Pressure Dynamic Burning Rate of Solid Propellants
A new method for determining the burning rate of a solid propellant, called the Impulse Method, is proposed in this paper. It is based on the proportional relationship between the impulse generated and the mass of the burned propellant. The pressure–time
Jiahao Liu +3 more
doaj +1 more source
Analysis of viscoelastic behavior of a filled elastomer under action of different loads [PDF]
Mechanical properties of viscoelastic filled polymers strongly depend on temperature and strain rate and vary for several orders of magnitude. During service life, a viscoelastic body, especially carboxy-terminated polybutadiene (CTPB) composite solid ...
Gligorijević Nikola I. +6 more
doaj +1 more source
Effect of Microstructure on Micro-Mechanical Properties of Composite Solid Propellant
This study was aimed at determining the effect of microstructure on the macro-mechanical behavior of a composite solid propellant. The microstructure model of a composite solid propellant was generated using molecular dynamics algorithm.
Tianpeng Li +3 more
doaj +1 more source

