Direct Simulation Monte Carlo Simulation of the Effect of Needle Valve Structures on the Rarefied Flow of Cold Gas Thrusters

The needle valve, serving as the flow control unit of the thruster system, is a crucial component of the entire thruster. Its performance directly impacts the flow state of the rarefied gas in the micro-nozzle structure of the cold gas micro-thruster, thereby exerting a significant influence on the...

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Main Authors: Songcai Lu, Xuhui Liu, Xudong Wang, Shurui Zhang, Yusong Yu, Yong Li
Format: Article
Language:English
Published: MDPI AG 2023-08-01
Series:Micromachines
Subjects:
Online Access:https://www.mdpi.com/2072-666X/14/8/1585
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author Songcai Lu
Xuhui Liu
Xudong Wang
Shurui Zhang
Yusong Yu
Yong Li
author_facet Songcai Lu
Xuhui Liu
Xudong Wang
Shurui Zhang
Yusong Yu
Yong Li
author_sort Songcai Lu
collection DOAJ
description The needle valve, serving as the flow control unit of the thruster system, is a crucial component of the entire thruster. Its performance directly impacts the flow state of the rarefied gas in the micro-nozzle structure of the cold gas micro-thruster, thereby exerting a significant influence on the high precision and stability of the propulsion system as a whole. This study examines the impact of different needle valve structures on the flow and thrust in micro-nozzles using the DSMC method. The analysis includes discussions on the spatial distribution, Kn distribution, slip velocity distribution, and pressure distribution of the micro-nozzle’s flow mechanism. Notably, increased curvature of the needle valve enhances the flow velocity in the throat and expansion section. The magnitude of the curvature directly affects the flow velocity, with larger curvatures resulting in higher velocities. Comparing different spool shapes, the conical spool shape minimizes the velocity gradient in the high-speed region at the junction between the spool area and the outlet pipe, particularly with a wide opening. Increasing the curvature of the spool leads to a higher velocity in the expansion section. Consequently, an arc-shaped spool valve maximizes the nitrogen flow at the nozzle during wide openings, thereby enhancing thrust. These research findings serve as a valuable reference for the structural design of the needle valve in the micro-nozzle of the cold gas micro-thruster.
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spelling doaj.art-87ac507faabd4a6eb6343ccbd437f9c72023-11-19T02:14:00ZengMDPI AGMicromachines2072-666X2023-08-01148158510.3390/mi14081585Direct Simulation Monte Carlo Simulation of the Effect of Needle Valve Structures on the Rarefied Flow of Cold Gas ThrustersSongcai Lu0Xuhui Liu1Xudong Wang2Shurui Zhang3Yusong Yu4Yong Li5Beijing Institute of Control Engineering, Beijing 100190, ChinaBeijing Institute of Control Engineering, Beijing 100190, ChinaBeijing Institute of Control Engineering, Beijing 100190, ChinaHydrogen Energy and Space Propulsion Laboratory (HESPL), School of Mechanical, Electronic and Control Engineering, Beijing Jiaotong University, Beijing 100044, ChinaHydrogen Energy and Space Propulsion Laboratory (HESPL), School of Mechanical, Electronic and Control Engineering, Beijing Jiaotong University, Beijing 100044, ChinaBeijing Institute of Control Engineering, Beijing 100190, ChinaThe needle valve, serving as the flow control unit of the thruster system, is a crucial component of the entire thruster. Its performance directly impacts the flow state of the rarefied gas in the micro-nozzle structure of the cold gas micro-thruster, thereby exerting a significant influence on the high precision and stability of the propulsion system as a whole. This study examines the impact of different needle valve structures on the flow and thrust in micro-nozzles using the DSMC method. The analysis includes discussions on the spatial distribution, Kn distribution, slip velocity distribution, and pressure distribution of the micro-nozzle’s flow mechanism. Notably, increased curvature of the needle valve enhances the flow velocity in the throat and expansion section. The magnitude of the curvature directly affects the flow velocity, with larger curvatures resulting in higher velocities. Comparing different spool shapes, the conical spool shape minimizes the velocity gradient in the high-speed region at the junction between the spool area and the outlet pipe, particularly with a wide opening. Increasing the curvature of the spool leads to a higher velocity in the expansion section. Consequently, an arc-shaped spool valve maximizes the nitrogen flow at the nozzle during wide openings, thereby enhancing thrust. These research findings serve as a valuable reference for the structural design of the needle valve in the micro-nozzle of the cold gas micro-thruster.https://www.mdpi.com/2072-666X/14/8/1585cold gas micro-nozzlerarefied flowDSMC methodneedle valve opening ratiolarge length-to-diameter ratiomicro-channel
spellingShingle Songcai Lu
Xuhui Liu
Xudong Wang
Shurui Zhang
Yusong Yu
Yong Li
Direct Simulation Monte Carlo Simulation of the Effect of Needle Valve Structures on the Rarefied Flow of Cold Gas Thrusters
Micromachines
cold gas micro-nozzle
rarefied flow
DSMC method
needle valve opening ratio
large length-to-diameter ratio
micro-channel
title Direct Simulation Monte Carlo Simulation of the Effect of Needle Valve Structures on the Rarefied Flow of Cold Gas Thrusters
title_full Direct Simulation Monte Carlo Simulation of the Effect of Needle Valve Structures on the Rarefied Flow of Cold Gas Thrusters
title_fullStr Direct Simulation Monte Carlo Simulation of the Effect of Needle Valve Structures on the Rarefied Flow of Cold Gas Thrusters
title_full_unstemmed Direct Simulation Monte Carlo Simulation of the Effect of Needle Valve Structures on the Rarefied Flow of Cold Gas Thrusters
title_short Direct Simulation Monte Carlo Simulation of the Effect of Needle Valve Structures on the Rarefied Flow of Cold Gas Thrusters
title_sort direct simulation monte carlo simulation of the effect of needle valve structures on the rarefied flow of cold gas thrusters
topic cold gas micro-nozzle
rarefied flow
DSMC method
needle valve opening ratio
large length-to-diameter ratio
micro-channel
url https://www.mdpi.com/2072-666X/14/8/1585
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