Results 41 to 50 of about 12,705 (201)
Machine Learning for Thermodynamic States of Notional Nonideal Energetic Mixtures
. ABSTRACT Currently, modeling the thermodynamic states in the reaction zone of a detonating energetic mixture entails iteratively solving a set of coupled differential equations that require detailed material property information or models whose empirical parameters must be physically measured.
Sangeeth Balakrishnan +7 more
wiley +1 more source
ABSTRACT The most common binder used in composite rocket propellants is based on the pre‐polymer hydroxyl‐terminated polybutadiene (HTPB). It has been shown to have excellent mechanical properties and a long life once crosslinked, and studies have examined the kinetics of crosslinking and pot life of energetic formulations with HTPB.
Laurel Hilger +2 more
wiley +1 more source
Boosting Decomposition and Combustion of TKX‐50 and HTPB/TKX‐50 Propellants With NH2‐MIL‐88B(Fe) MOF
ABSTRACT Dihydroxylammonium 5,5′‐bistetrazole‐1,1′‐diolate (TKX‐50) is a promising energetic material that possesses both exceptional energy density and low sensitivity. Nevertheless, its application is hindered by incomplete pyrolysis during combustion or explosion. Various strategies, including eutectic formation, composite preparation, and catalysis,
Jingwen Chen +10 more
wiley +1 more source
Research on mechanical properties of HTPB propellants
Abstract Slat propellants with different sizes and shapes are designed to investigate the strength criteria of HTPB propellants. According to the calculation and simulation results, with the increase of multiple, the designed size slat specimens can achieve equivalent biaxial tensile stress ratios of 1:2, 1:2.5, 1:3, 1:3.5, and 1:4 under
Chang Liu +4 more
openaire +1 more source
Aging of the Binders GAP-N100 and HTPB-IPDI investigated by Torsion-DMA
S.199-205The aging of the binders GAP‐N100 and HTPB‐IPDI was investigated by DMA in torsion mode to find out the changes in the storage shear modulus G'(o), loss shear modulus G"(o) and in the glass transition temperature TG.
Bohn, Manfred, Elsner, Peter
core +1 more source
ABSTRACT We report on the synthesis and characterization of 3‐(2‐(2‐azidoethoxy)ethoxy)‐4‐nitro‐1,2,5‐oxadiazole (NFPEG2N3), which is a liquid nitrofurazanyl ether that was designed to be an energy‐rich plasticizer for glycidyl azide polymer (GAP)‐ and nitrocellulose (NC)‐based formulations.
P. Lieber +3 more
wiley +1 more source
The Effects of Density on Burning Rates of AP/HTPB Composite Solid Propellants [PDF]
Within identical composite solid AP/HTPB propellant formulations, the densities of each individual propellant can greatly vary depending on their manufacturing quality.
Hong, Alvin
core +1 more source
Nitrate ester functionalized ionic liquid as energetic plasticizer for HTPB propellant
Energetic plasticizers are rarely used in HTPB propellants due to compatibility issues; one strategy is usually adopted is to introduce energetic substituents.
Ze Su +6 more
doaj +1 more source
In order to study the macroscopic mechanical properties and meso damage mechanism of solid fuel hydroxy-terminated polybutadiene (HTPB) propellant under low temperature and dynamic biaxial compression loading, the INSTRON high strain rate hydraulic ...
Tingjing Geng +5 more
doaj +1 more source
Biaxial Tensile Mechanical Properties of HTPB Solid Propellant
The purpose of this work is to study the effects of different loading rate ratios and loading speeds on the biaxial tension of hydroxyl-terminated polybutadiene (HTPB) solid propellant. A proper kind of biaxial tensile specimen with which the stresses in its central part can be obtained with the loads acted on each loading direction is designed and ...
Li Jin +3 more
openaire +2 more sources

