Results 1 to 10 of about 360 (164)
Research on curing reaction kinetics and curing process of hydroxy-terminated polybutadiene (HTPB) propellants [PDF]
Hydroxyl-terminated polybutadiene (HTPB) propellants are high-performance solid propellants widely used in aerospace and military applications. By combining experimental and theoretical approaches, the curing process was analyzed using differential ...
Zhiming Guo +7 more
doaj +2 more sources
Solid propellants: AP/HTPB composite propellants
AbstractIn this article we mainly discuss about AP/HTPB composite solid propellants. Classification, components, properties, burning rate and ignition behavior of propellants are mentioned here. Combustion of AP monopropellant, HTPB and AP/HTPB is discussed in detail.
Pragnesh N Dave, Shalini Chaturvedi
exaly +2 more sources
First applications of ultrasound technology in solid rocket propellant combustion promotion [PDF]
The regulation of propellant combustion using ultrasonic waves is proposed. Under ultrasonic frequencies of 25–40 kHz, we systematically examined the combustion characteristics of Al particles, ammonium perchlorate (AP)/hydroxyl-terminated polybutadiene (
Zhan Wen +6 more
doaj +2 more sources
Study on Creep Mechanical Properties of HTPB Solid Propellant. [PDF]
Solid rocket propellants based on hydroxyl-terminated polybutadiene (HTPB), in which HTPB acts as the polymeric binder and fuel matrix, are widely used in aerospace propulsion. During storage, transport, and service, these composite energetic materials are exposed to sustained mechanical loads as well as environmental variations, which may induce time ...
Jin L, Jia S, Zhang Z, An Z, Lu Z.
europepmc +2 more sources
Combustion and mechanical properties enhancement strategy based on stearic acid surface activated boron powders [PDF]
Boric acid and other impurities on the surface of boron (B) particles can interact with hydroxyl-terminated polybutadiene (HTPB), weakening the mechanical properties and energy release efficiency of boron-based solid rocket propellants.
Jiaxin Lu +5 more
doaj +2 more sources
Preliminary Study on Characteristics of NC/HTPB-Based High-Energy Gun Propellants
This study mainly explored the characteristics of NC/HTPB-based high-energy gun propellants with RDX, CL-20 or TKX-50 by experimental method. Three series of test samples were prepared referring to the formulation of M1 single-base gun propellant (M1 SBP)
Yi-Hsien Lin +4 more
doaj +1 more source
In order to solve the problem of weak injection of fuel-rich propellant and to enhance its burning rate, the combustion behaviors of Al/Mg-based fuel-rich HTPB propellants with 40wt% metal content were studied with and without the addition of fast ...
Han Shi +4 more
doaj +1 more source
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
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
The interfacial interaction between the main oxidant filler ammonium perchlorate (AP) and hydroxyl-terminated polybutadiene (HTPB) matrix in AP/HTPB propellants were studied via an all-atom molecular dynamics simulation.
Dong Ge +6 more
doaj +1 more source

