Research graph
References from Mechanisms of combustion instability in MEMS solid-propellant microthrusters under transient depressurization. Local targets link to admitted publications; unresolved targets remain external evidence.
Space micropropulsion systems for Cubesats and small satellites: from proximate targets to furthermost frontiers
10.1063/1.5007734 · 2018 · External reference
Large constellations of small satellites: a survey of near future challenges and missions
10.3390/aerospace7090133 · 2020 · External reference
A review on solid propellant micro-thruster array based on MEMS technology
10.1016/j.fpc.2023.03.002 · 2024 · External reference
Recent advances in MEMS-based microthrusters
10.3390/mi10120818 · 2019 · External reference
Extinction of AP monopropellant by rapid depressurization: computational and experimental studies
10.1016/j.combustflame.2017.05.030 · 2017 · External reference
Investigation on the ignition of a MEMS solid propellant microthruster before propellant combustion
10.1088/0960-1317/17/2/019 · 2007 · External reference
A MEMS-based solid propellant microthruster with Au/Ti igniter
10.1016/j.sna.2005.04.021 · 2005 · External reference
MEMS-based solid propellant microthruster design, simulation, fabrication, and testing
10.1109/jmems.2004.825309 · 2004 · External reference
Flame structure and burning rate of ammonium perchlorate/hydroxyl-terminated polybutadiene propellant sandwiches
10.1016/s0082-0784(00)80289-1 · 2000 · External reference
AP/HTPB laminate propellant flame structure: Fuel-lean intrinsic instability
10.1016/j.proci.2006.07.131 · 2007 · External reference
Homogenization issues and the combustion of heterogeneous solid propellants
10.1016/s1540-7489(02)80357-1 · 2002 · External reference
Diffusion flame calculations for composite propellants predicting particle-size effects
10.1016/j.combustflame.2009.09.004 · 2010 · External reference
Theoretical study of the flame describing function of AP/HTPB propellant flame based on sandwich model
10.1016/j.actaastro.2019.06.009 · 2019 · External reference
Eulerian thermo-mechanical simulations of heterogeneous solid propellants using an approximate projection method
10.1016/j.combustflame.2020.05.023 · 2020 · External reference
Unsteady heat and mass transfer mechanism in AP/HTPB propellant combustion under rapid depressurization
10.1016/j.icheatmasstransfer.2023.106949 · 2023 · External reference
Chemical behavior research of high-energy aerospace propellant with a mesoscale heterogeneous packing model
10.1016/j.cej.2024.150430 · 2024 · External reference
Combustion performance modulation and agglomeration inhibition of HTPB propellants by fine Al/oxidizers integration
10.1016/j.fuel.2024.131587 · 2024 · External reference
Highly energy release of aluminum@ammonium perchlorate composites incorporated with graphene oxide-based energetic coordination polymer
2025 · External reference
Enhancing the ignition and combustion performances of solid propellants incorporating Al particles inside oxidizers
10.1021/acsami.3c11961 · 2023 · External 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 · 2024 · External reference
Lab-on-PCB solid propellant microthruster with multi-mode thrust capabilities
10.1039/d4lc00516c · 2024 · External reference
Design and fabrication of a scalable solid-propellant micro-thruster array using lab-on-PCB technology
10.1016/j.sna.2023.114738 · 2023 · External reference
Random packing of heterogeneous propellants
10.2514/2.1361 · 2001 · External reference
Nonsteady burning of periodic sandwich propellants with complete coupling between the solid and gas phases
10.1016/s0010-2180(01)00226-7 · 2001 · External reference
Coupled simulation of fluid flow and propellant burning surface regression in a solid rocket motor
10.1016/j.compfluid.2014.01.028 · 2014 · External reference
Accurate computation of grain burning coupled with flow simulation in rocket chamber
10.2514/1.b35736 · 2015 · External reference
Estimation of surface geometry on combustion characteristics of AP/HTPB propellant under rapid depressurization
10.1016/j.dt.2023.07.019 · 2024 · External reference
Analysis on ignition kernel formation in a quiescent mixture: different characteristic time scales and critical heating powers
10.1016/j.combustflame.2022.112336 · 2022 · External reference
Micro-flow properties of NEPE propellant in a rotating depressurization combustion environment of solid rocket motor
10.1016/j.ast.2024.109354 · 2024 · External reference
