利用外磁场增强固体推进剂的燃烧性能

IF 5.8 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2025-04-01 Epub Date: 2025-02-06 DOI:10.1016/j.ast.2025.110013
Songchen Yue , Geng Xu , Linchen Dai , Wei Liu , Meng Cui , Shiyao Shao , Peijin Liu , Wen Ao
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引用次数: 0

摘要

推进剂在磁场下的燃烧显示出巨大的发展潜力。本研究探讨了利用磁场改善固体复合推进剂燃烧性能的潜力。实验装置包括一个定制的装置,可以调节磁场的强度和方向,以及激光点火装置。研究表明,施加磁场可缩短点火延迟时间,加快燃烧速度,提高推进剂的燃烧效率。具体来说,施加196 mT磁场将点火延迟时间从493.08 ms减少到483.68 ms,燃烧速率从2.41 mm/s增加到2.86 mm/s,燃烧效率从82.65%提高到90.15%。比冲由2315 N·s/kg提高到2347 N·s/kg。在氧化剂含量较高的推进剂中,磁场的影响更为明显。然而,当燃烧方向与磁场方向垂直时,影响略有减弱。进一步研究了该推进剂在磁场作用下的燃烧物理机理。结果表明,磁场通过减少铝颗粒的点火延迟时间和降低火焰高度来促进推进剂的燃烧。这一发现为提高推进剂性能提供了有希望的见解。
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Enhancing the combustion performance of solid propellants by external magnetic field
Propellant combustion under a magnetic field demonstrates significant potential for advancement. This study explores the potential of using magnetic fields to improve combustion performance of solid composite propellants. The experimental setup involved a custom-made apparatus that could adjust the intensity and direction of the magnetic field and laser ignition device. The research demonstrated that applying a magnetic field shortened the ignition delay time, accelerated the burning rate, and improved the propellant's combustion efficiency. Specifically, applying a 196 mT magnetic field reduces ignition delay time from 493.08 ms to 483.68 ms, increased the burning rate from 2.41 mm/s to 2.86 mm/s, and raised combustion efficiency from 82.65 % to 90.15 %. Specific impulse also improved from 2315 N·s/kg to 2347 N·s/kg. The magnetic field's effect was more pronounced in propellants with higher oxidizer content. However, when combustion was perpendicular to the magnetic field direction, the influence slightly diminished. We further investigated the combustion physical mechanism of the propellant under the influence of a magnetic field. The results demonstrate that the magnetic field enhances propellant combustion by reducing the ignition delay time of aluminum particles and lowering the flame height. This discovery offers promising insights for enhancing propellant performance.
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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