Solid rocket motor in-line ignition system design

Shi Wei Yuan

Solid rocket motor in-line ignition system design

Shi Wei Yuan^*

^*此作品的通讯作者

宇航学院

科研成果: 期刊稿件 › 文章 › 同行评审

1 引用（Scopus）

摘要

In-line ignition system and its corresponded U.S.A military standard are introduced. Advantages and domestic study situation are mentioned. Detail designed slapper igniter which direct to igniting boron/potassium nitrate (BPN) is finish. Preliminary numerical simulation on slapper flying plate velocity result is 3500 m/s. Experiment shows design is success and BPN can be igniting under that velocity.

源语言	英语
页（从-至）	1059-1062+1067
期刊	Yuhang Xuebao/Journal of Astronautics
卷	27
期	5
出版状态	已出版 - 9月 2006

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引用此

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title = "Solid rocket motor in-line ignition system design",

abstract = "In-line ignition system and its corresponded U.S.A military standard are introduced. Advantages and domestic study situation are mentioned. Detail designed slapper igniter which direct to igniting boron/potassium nitrate (BPN) is finish. Preliminary numerical simulation on slapper flying plate velocity result is 3500 m/s. Experiment shows design is success and BPN can be igniting under that velocity.",

keywords = "Boron/potassium nitrate (BPN), In-line ignition, Micro-pulse power device, Slapper igniter, Solid rocket motor",

author = "Yuan, \{Shi Wei\}",

year = "2006",

month = sep,

language = "英语",

volume = "27",

pages = "1059--1062+1067",

journal = "Yuhang Xuebao/Journal of Astronautics",

issn = "1000-1328",

publisher = "Chinese Society of Astronautics",

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T1 - Solid rocket motor in-line ignition system design

AU - Yuan, Shi Wei

PY - 2006/9

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N2 - In-line ignition system and its corresponded U.S.A military standard are introduced. Advantages and domestic study situation are mentioned. Detail designed slapper igniter which direct to igniting boron/potassium nitrate (BPN) is finish. Preliminary numerical simulation on slapper flying plate velocity result is 3500 m/s. Experiment shows design is success and BPN can be igniting under that velocity.

AB - In-line ignition system and its corresponded U.S.A military standard are introduced. Advantages and domestic study situation are mentioned. Detail designed slapper igniter which direct to igniting boron/potassium nitrate (BPN) is finish. Preliminary numerical simulation on slapper flying plate velocity result is 3500 m/s. Experiment shows design is success and BPN can be igniting under that velocity.

KW - Boron/potassium nitrate (BPN)

KW - In-line ignition

KW - Micro-pulse power device

KW - Slapper igniter

KW - Solid rocket motor

UR - https://www.scopus.com/pages/publications/33846071603

M3 - 文章

AN - SCOPUS:33846071603

SN - 1000-1328

VL - 27

SP - 1059-1062+1067

JO - Yuhang Xuebao/Journal of Astronautics

JF - Yuhang Xuebao/Journal of Astronautics

IS - 5

ER -

Solid rocket motor in-line ignition system design

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