Rocket Motor Igniter, Arming Firing Device

机译：火箭发动机点火器，布防点火装置

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摘要

This invention illustrates an arming-firing means that can be utilized with many guided missile systems. The utilization of a safe arming-firing device that is compatible with many guided missile systems is an absolute necessity in view of accidental ignition frequency. (Author)

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作者
Hibbs, J. E.; Chalmers, G. W.; Durrell, R. R.; Smith, W. C.;
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年度 1979
页码 p.1-17
总页数 17
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Patent applications; Rocket engines; Arming devices; Guided missile components; Inventions; Rocket igniters; Guided missiles; Guided missile safety;

机译：专利申请;火箭发动机;装备;导弹部件;发明;火箭点火器;导弹;导弹安全;

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1. Combustion characterization of a CH_4/O_2 rapid mixed swirl torch igniter for hybrid rocket motors [J] . Aerospace science and technology . 2020,第Mara期

机译：混合火箭发动机CH_4 / O_2快速混合旋流火炬点火器的燃烧特性
2. A Model for Igniter Mass Flow Rate History Evaluation for Solid Rocket Motors [J] . Ma Yanjie, Bao Futing, Hui Weihua, International journal of aerospace engineering . 2019,第PTa5期

机译：固体火箭电动机点火器质量流量历史评估模型
3. A Model for Igniter Mass Flow Rate History Evaluation for Solid Rocket Motors [J] . Yanjie Ma, Futing Bao, Weihua Hui, International journal of aerospace engineering . 2019,第4期

机译：固体火箭电动机点火器质量流量历史评估模型
4. DESIGN ASPECTS OF HEAD END MOUNTED SAFE ARM (HMSA) FOR IGNITERS OF SOLID ROCKET MOTORS [C] . Rajesh Mathew, Yezhil Arasu, Thomas Kurian, International Astronautical Congress . 2015

机译：用于稳固火箭电机的点火器的头端安装安全臂（HMSA）的设计方面
5. FILM COOLING OF ROCKET MOTORS: PART I: AN EXPERIMENTAL AND THEORETICAL INVESTIGATION OF FILM COOLING OF ROCKET MOTORS PART II: FILM COOLING, ITSTHEORY AND APPLICATIONS. [D] . GRAHAM, ALFRED RAPP. 1958

机译：火箭发动机薄膜冷却：第一部分：火箭发动机薄膜冷却的实验和理论研究第二部分：薄膜冷却，其理论和应用。
6. Preferences for Firearm Locking Devices and Device Features Among Participants in a Firearm Safety Event [O] . Joseph A. Simonetti, Cassie Simeona, Chelsie Gallagher, 2019

机译：枪支安全事件参与者中枪支锁定设备和设备功能的首选项
7. Influence of the ignition mixture particle size on rocket motor igniter pressure gradient [O] . Nikola Gligorijević, Jovica Nešić, Jovica Bogdanov, 2018

机译：火箭电机点火器压力梯度对火箭混合粒径的影响
8. Rocket Motor Igniter, Arming Firing Device. [R] . Hibbs, J. E., Chalmers, G. W., Durrell, R. R., 1979

机译：火箭发动机点火器，布防点火装置。

Rocket Motor Igniter, Arming Firing Device

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