Research on Interior Ballistic of a Gas Multi-stage Cylinder Ejection

Mei Huang; Yi Jiang; Boman Wang

doi:10.1051/matecconf/201817903005

Research on Interior Ballistic of a Gas Multi-stage Cylinder Ejection

Mei Huang^*
, Yi Jiang
, Boman Wang

^*此作品的通讯作者

空天科学与技术学院

Beijing Institute of Technology

科研成果: 期刊稿件 › 会议文章 › 同行评审

3 引用（Scopus）

摘要

Aimed at increasing aircraft's leaving speed based on a determinate length of aircraft container and ensuring the aircraft's acceleration below one certain value, a new gas multi-stage cylinder ejection is proposed in this paper, and at the same time the primary design and the interior ballistic evaluating are processed. The simulation results can be used for the design of gas-catapult device and provide theoretical support for parameter optimizations in trajector.

源语言	英语
文章编号	03005
期刊	MATEC Web of Conferences
卷	179
DOI	https://doi.org/10.1051/matecconf/201817903005
出版状态	已出版 - 26 7月 2018
活动	2018 2nd International Conference on Mechanical, Material and Aerospace Engineering, 2MAE 2018 - Wuhan, 中国期限: 10 5月 2018 → 13 5月 2018

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10.1051/matecconf/201817903005

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引用此

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title = "Research on Interior Ballistic of a Gas Multi-stage Cylinder Ejection",

abstract = "Aimed at increasing aircraft's leaving speed based on a determinate length of aircraft container and ensuring the aircraft's acceleration below one certain value, a new gas multi-stage cylinder ejection is proposed in this paper, and at the same time the primary design and the interior ballistic evaluating are processed. The simulation results can be used for the design of gas-catapult device and provide theoretical support for parameter optimizations in trajector.",

author = "Mei Huang and Yi Jiang and Boman Wang",

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year = "2018",

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T1 - Research on Interior Ballistic of a Gas Multi-stage Cylinder Ejection

AU - Huang, Mei

AU - Jiang, Yi

AU - Wang, Boman

PY - 2018/7/26

Y1 - 2018/7/26

N2 - Aimed at increasing aircraft's leaving speed based on a determinate length of aircraft container and ensuring the aircraft's acceleration below one certain value, a new gas multi-stage cylinder ejection is proposed in this paper, and at the same time the primary design and the interior ballistic evaluating are processed. The simulation results can be used for the design of gas-catapult device and provide theoretical support for parameter optimizations in trajector.

AB - Aimed at increasing aircraft's leaving speed based on a determinate length of aircraft container and ensuring the aircraft's acceleration below one certain value, a new gas multi-stage cylinder ejection is proposed in this paper, and at the same time the primary design and the interior ballistic evaluating are processed. The simulation results can be used for the design of gas-catapult device and provide theoretical support for parameter optimizations in trajector.

UR - https://www.scopus.com/pages/publications/85063178372

U2 - 10.1051/matecconf/201817903005

DO - 10.1051/matecconf/201817903005

M3 - Conference article

AN - SCOPUS:85063178372

SN - 2261-236X

VL - 179

JO - MATEC Web of Conferences

JF - MATEC Web of Conferences

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T2 - 2018 2nd International Conference on Mechanical, Material and Aerospace Engineering, 2MAE 2018

Y2 - 10 May 2018 through 13 May 2018

ER -

Research on Interior Ballistic of a Gas Multi-stage Cylinder Ejection

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