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Zuyan Wu, Zhenwei Ye, Taotao Liu, Chenhao Yu
Abstract
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Confidence 100%
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Confidence 95%
No local reference links have been materialized yet.
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Space micropropulsion systems for Cubesats and small satellites: from proximate targets to furthermost frontiers
10.1063/1.5007734 · 2018
Large constellations of small satellites: a survey of near future challenges and missions
10.3390/aerospace7090133 · 2020
A review on solid propellant micro-thruster array based on MEMS technology
10.1016/j.fpc.2023.03.002 · 2024
Recent advances in MEMS-based microthrusters
10.3390/mi10120818 · 2019
Extinction of AP monopropellant by rapid depressurization: computational and experimental studies
10.1016/j.combustflame.2017.05.030 · 2017
Investigation on the ignition of a MEMS solid propellant microthruster before propellant combustion
10.1088/0960-1317/17/2/019 · 2007
A MEMS-based solid propellant microthruster with Au/Ti igniter
10.1016/j.sna.2005.04.021 · 2005
MEMS-based solid propellant microthruster design, simulation, fabrication, and testing
10.1109/jmems.2004.825309 · 2004
Flame structure and burning rate of ammonium perchlorate/hydroxyl-terminated polybutadiene propellant sandwiches
10.1016/s0082-0784(00)80289-1 · 2000
datacite
Confidence 0%
AP/HTPB laminate propellant flame structure: Fuel-lean intrinsic instability
10.1016/j.proci.2006.07.131 · 2007
Homogenization issues and the combustion of heterogeneous solid propellants
10.1016/s1540-7489(02)80357-1 · 2002
Diffusion flame calculations for composite propellants predicting particle-size effects
10.1016/j.combustflame.2009.09.004 · 2010
Theoretical study of the flame describing function of AP/HTPB propellant flame based on sandwich model
10.1016/j.actaastro.2019.06.009 · 2019
Eulerian thermo-mechanical simulations of heterogeneous solid propellants using an approximate projection method
10.1016/j.combustflame.2020.05.023 · 2020
Unsteady heat and mass transfer mechanism in AP/HTPB propellant combustion under rapid depressurization
10.1016/j.icheatmasstransfer.2023.106949 · 2023
Chemical behavior research of high-energy aerospace propellant with a mesoscale heterogeneous packing model
10.1016/j.cej.2024.150430 · 2024
Combustion performance modulation and agglomeration inhibition of HTPB propellants by fine Al/oxidizers integration
10.1016/j.fuel.2024.131587 · 2024
Highly energy release of aluminum@ammonium perchlorate composites incorporated with graphene oxide-based energetic coordination polymer
2025
Enhancing the ignition and combustion performances of solid propellants incorporating Al particles inside oxidizers
10.1021/acsami.3c11961 · 2023
Control of burning rate pressure sensitivity for solid propellants by changing the interfacial contact of Al/HMX/AP with precisely located graphene-based energetic catalysts
10.1016/j.combustflame.2024.113665 · 2024
Lab-on-PCB solid propellant microthruster with multi-mode thrust capabilities
10.1039/d4lc00516c · 2024
Design and fabrication of a scalable solid-propellant micro-thruster array using lab-on-PCB technology
10.1016/j.sna.2023.114738 · 2023
Random packing of heterogeneous propellants
10.2514/2.1361 · 2001
Nonsteady burning of periodic sandwich propellants with complete coupling between the solid and gas phases
10.1016/s0010-2180(01)00226-7 · 2001
Coupled simulation of fluid flow and propellant burning surface regression in a solid rocket motor
10.1016/j.compfluid.2014.01.028 · 2014
Accurate computation of grain burning coupled with flow simulation in rocket chamber
10.2514/1.b35736 · 2015
Estimation of surface geometry on combustion characteristics of AP/HTPB propellant under rapid depressurization
10.1016/j.dt.2023.07.019 · 2024
Analysis on ignition kernel formation in a quiescent mixture: different characteristic time scales and critical heating powers
10.1016/j.combustflame.2022.112336 · 2022
Micro-flow properties of NEPE propellant in a rotating depressurization combustion environment of solid rocket motor
10.1016/j.ast.2024.109354 · 2024
Micro-flow properties of NEPE propellant in a rotating depressurization combustion environment of solid rocket motor
10.1016/j.ast.2024.109354 · doi-reference
Analysis on ignition kernel formation in a quiescent mixture: different characteristic time scales and critical heating powers
10.1016/j.combustflame.2022.112336 · doi-reference
Estimation of surface geometry on combustion characteristics of AP/HTPB propellant under rapid depressurization
10.1016/j.dt.2023.07.019 · doi-reference
Accurate computation of grain burning coupled with flow simulation in rocket chamber
10.2514/1.b35736 · doi-reference
Coupled simulation of fluid flow and propellant burning surface regression in a solid rocket motor
10.1016/j.compfluid.2014.01.028 · doi-reference
Nonsteady burning of periodic sandwich propellants with complete coupling between the solid and gas phases
10.1016/s0010-2180(01)00226-7 · doi-reference
Random packing of heterogeneous propellants
10.2514/2.1361 · doi-reference
Design and fabrication of a scalable solid-propellant micro-thruster array using lab-on-PCB technology
10.1016/j.sna.2023.114738 · doi-reference
Lab-on-PCB solid propellant microthruster with multi-mode thrust capabilities
10.1039/d4lc00516c · doi-reference
Control of burning rate pressure sensitivity for solid propellants by changing the interfacial contact of Al/HMX/AP with precisely located graphene-based energetic catalysts
10.1016/j.combustflame.2024.113665 · doi-reference
Enhancing the ignition and combustion performances of solid propellants incorporating Al particles inside oxidizers
10.1021/acsami.3c11961 · doi-reference
Combustion performance modulation and agglomeration inhibition of HTPB propellants by fine Al/oxidizers integration
10.1016/j.fuel.2024.131587 · doi-reference
Chemical behavior research of high-energy aerospace propellant with a mesoscale heterogeneous packing model
10.1016/j.cej.2024.150430 · doi-reference
Unsteady heat and mass transfer mechanism in AP/HTPB propellant combustion under rapid depressurization
10.1016/j.icheatmasstransfer.2023.106949 · doi-reference
Eulerian thermo-mechanical simulations of heterogeneous solid propellants using an approximate projection method
10.1016/j.combustflame.2020.05.023 · doi-reference
Theoretical study of the flame describing function of AP/HTPB propellant flame based on sandwich model
10.1016/j.actaastro.2019.06.009 · doi-reference
Diffusion flame calculations for composite propellants predicting particle-size effects
10.1016/j.combustflame.2009.09.004 · doi-reference
Homogenization issues and the combustion of heterogeneous solid propellants
10.1016/s1540-7489(02)80357-1 · doi-reference
AP/HTPB laminate propellant flame structure: Fuel-lean intrinsic instability
10.1016/j.proci.2006.07.131 · doi-reference
Flame structure and burning rate of ammonium perchlorate/hydroxyl-terminated polybutadiene propellant sandwiches
10.1016/s0082-0784(00)80289-1 · doi-reference
MEMS-based solid propellant microthruster design, simulation, fabrication, and testing
10.1109/jmems.2004.825309 · doi-reference
A MEMS-based solid propellant microthruster with Au/Ti igniter
10.1016/j.sna.2005.04.021 · doi-reference
Investigation on the ignition of a MEMS solid propellant microthruster before propellant combustion
10.1088/0960-1317/17/2/019 · doi-reference
Extinction of AP monopropellant by rapid depressurization: computational and experimental studies
10.1016/j.combustflame.2017.05.030 · doi-reference
Recent advances in MEMS-based microthrusters
10.3390/mi10120818 · doi-reference
A review on solid propellant micro-thruster array based on MEMS technology
10.1016/j.fpc.2023.03.002 · doi-reference
Large constellations of small satellites: a survey of near future challenges and missions
10.3390/aerospace7090133 · doi-reference
Space micropropulsion systems for Cubesats and small satellites: from proximate targets to furthermost frontiers
10.1063/1.5007734 · doi-reference