Results 221 to 230 of about 52,081 (256)

Graphene oxide-(ferrocenylmethyl) dimethylammonium 3-nitro-1,2,4-triazol-5-one composites as catalysts on the combustion of HTPB propellant

Combustion and Flame, 2023
Yonghu Zhu, Liping Jiang, Xiaolong Fu, R. Shen, Lizhi Wu   +4 more
semanticscholar   +1 more source

Microflame diffusion properties of AP/HTPB propellant under binder width effects

Journal of Mechanical Science and Technology, 2023
Kaixuan Chen, Xiaochun Xue, Yonggang Yu, Zhenwei Ye   +3 more
semanticscholar   +1 more source

Unsteady heat and mass transfer mechanism in AP/HTPB propellant combustion under rapid depressurization

International Communications in Heat and Mass Transfer, 2023
Kai Chen, Zhenwei Ye, Yizhe Yu, Xiaochun Xue, Yonggang Yu   +4 more
semanticscholar   +1 more source

Aging of HTPB Propellant

41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2005
Moshe Kivity, Gadi Hartman, Abraham Achlama   +2 more
openaire   +1 more source

Experimental Investigation on Fracture Properties of HTPB Propellant with Circumferentially Notched Cylinder Sample

Propellants, explosives, pyrotechnics, 2022
Zhejun Wang, H. Qiang, Jiaxiang Wang, Leiguang Duan   +3 more
semanticscholar   +1 more source

Aging Characteristics of HTPB Propellant Based on Volume Resistivity

Propellants, Explosives, Pyrotechnics
ABSTRACTHydroxyl‐terminated polybutadiene (HTPB) propellant faces the problem of aging from casting to use. Generally, the aging degree of HTPB propellant is evaluated by a destructive mechanical property test. Therefore, it is necessary to seek a new evaluation method. Electrical performance is a method that can achieve nondestructive testing. However,
Lina Xie, Kaifeng Lin, Wenlong Huo, Xueying Sun, Xuhui Chi, Chengyuan Zhao, Fengtao Zhang, Junzhuo Li, Yulin Yang, Debin Xia, Jian Zhang   +10 more
openaire   +1 more source

A Study of a Novel Additive for HTPB Propellant

1976
Abstract : Experimental studies were conducted to define the utility regimes of graphite linters (chopped graphite fiber ranging from 50 to 200 micrometers) with respect to burn rate augmentation, acoustic stabilization and processing improvement in HTPB composite propellant. Linter utility regimes were defined with respect to burn rate reproducibility
M. W. Beckstead, A. G. Butcher, J. P. Peterson   +2 more
openaire   +1 more source

HTPB propellant aging and service life

16th Joint Propulsion Conference, 1980
A. CHRISTIANSEN, L. LAYTON, R. CARPENTER
openaire   +1 more source

Friction-induced ignition study of HTPB propellant based on a coupled chemo-mechano-thermodynamic model under ultrahigh acceleration overload conditions

Case Studies in Thermal Engineering, 2023
Ran Wang, Ningfei Wang, Jun Gao, Yiming Zhang, Anni Zhang, Yi Wu   +5 more
semanticscholar   +1 more source

Development of HTPB binder for solid propellant

24th Joint Propulsion Conference, 1988
KATSUAKI KOSAKA, SHIGERU SUZUKI, DAIZO FUKUMA, AKIHIKO YAMAMOTO, HARUKI MARUIZUMI   +4 more
openaire   +1 more source