Results 111 to 120 of about 988 (214)

Investigation of the agglomeration reduction mechanism of the aluminized HTPB propellant containing ferric perfluorooctanoate [Fe(PFO)₃]. [PDF]

RSC Adv, 2019
Zhen F, Zhou X, Zou M, Meng L, Yang R, Wang L, Huang F, Li J.   +7 more
europepmc   +1 more source

Constant Strain Aging Model of HTPB Propellant Involving Thermal–Mechanical Coupled Effects

To investigate the aging behavior of HTPB composite solid propellant under constant strain conditions, this study analyzed the aging patterns of the propellant’s maximum elongation at four temperatures (323.15 K–343.15 K) and five strain ...
Jiming Cheng, Kai Jiang, Pengju Qin, Xiangyu Zhang   +3 more
core   +1 more source

Characteristics of HTPB/AP/AOT Solid Propellant

Journal of the Korean Society of Propulsion Engineers, 2018
Miri Kim, Jaesung Choi, Jeongeun Kim, Myungpyo Hong, Hyoungjin Lee   +4 more
openaire   +1 more source

Effects of aluminum and iron nanoparticle additives on composite AP/HTPB solid propellant regression rate

, 2014
This project was started in the interest of supplementing existing data on additives to composite solid propellants. The study on the addition of iron and aluminum nanoparticles to composite AP/HTPB propellants was conducted at the Combustion and Energy ...
Styborski, Jeremy A.
core   +1 more source

Experimental Study on the Evolution of Mechanical Properties and Their Mechanisms in a HTPB Propellant Under Fatigue Loading. [PDF]

Polymers (Basel)
Feng F, Chen X, Xu J, Zeng Y, Huang W, Dong J.   +5 more
europepmc   +1 more source

Integrated Experimental-Numerical Analysis of HTPB Propellant Casting Optimization and Droplet Dynamics. [PDF]

ACS Omega
Guo Z, Rossi R, Xue Y, Wu Y, Fu X.
europepmc   +1 more source

Preparation of mono-dispersed, high energy release, core/shell structure Al nanopowders and their application in HTPB propellant as combustion enhancers. [PDF]

Sci Rep, 2017
Wang F, Wu Z, Shangguan X, Sun Y, Feng J, Li Z, Chen L, Zuo S, Zhuo R, Yan P.   +9 more
europepmc   +1 more source

Effect of HTPB Polymer Characteristics on Propellant Performance

Effect of HTPB Polymer Characteristics on Propellant Performance
資料番号 ...
openaire  

Multi-Objective Optimization of Damage Volume and CO₂ Consumption for High-Pressure Liquid CO₂ Jet Impact on Hydroxyl-Terminated Polybutadiene Propellant. [PDF]

Materials (Basel)
Zhang Z, Jiang D, Bai Y, Zhang H, Ding Y.   +4 more
europepmc   +1 more source

Synthesis and UV-Curing Modification of the High cis-1,4-Hydroxyl-Terminated Polybutadiene Binder Suitable for Ultra-Low Temperature Applications. [PDF]

Polymers (Basel)
Lyu H, Wang L, Li Y, Yu G, Liu S, Sun D, Liang Y, Huo P, Zhang D, Ning Z, Kong X.   +10 more
europepmc   +1 more source