| 飞马座空间运载火箭的推进系统 |
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| 引用本文： | 徐涛清. 飞马座空间运载火箭的推进系统[J]. 固体火箭技术, 1993, 0(1): 20-24 |
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| 作者姓名： | 徐涛清 |
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| 作者单位： | 四院四十七所 西安710000 |
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| 摘 要： | 飞马座空间运载火箭的推进系统为三级固体推进剂火箭发动机,本文对发动机的设计、制造和试验作了全面介绍,重点讨论了三级发动机的设计特点,即为了提高系统可靠性和降低生产成本,采用大的设计安全系数和在其它型号上使用过的成熟技术。
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| 关 键 词： | 火箭发动机 复合材料 壳体 绝热层 |
Propulsion System for Pegasus Air-Launched Space Booster |
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| Xu Taoqing Institute No. of Research Academy No.,Xi'an.. Propulsion System for Pegasus Air-Launched Space Booster[J]. Journal of Solid Rocket Technology, 1993, 0(1): 20-24 |
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| Authors: | Xu Taoqing Institute No. of Research Academy No. Xi'an. |
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| Affiliation: | Xu Taoqing Institute No.47 of Research Academy No.4,Xi'an.710000 |
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| Abstract: | The propulsion system for the Pegasus air-launched space booster consists of three stage solid propellant rocket motors.The design,manufacture and tests of the motors are comprehensively presented,with emphasis on their design feature that a large safe fac- tor in design and demonstrated technologies are used for the system reliability improvement and cost reduction. |
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| Keywords: | Solid rocket engine Composite case Insulation Nozzle Pegasus air-launched space booster |
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