航天推进技术研究院主办
[1]耿文忠.新型液体火箭发动机试车台
起动试验系统方案设计[J].火箭推进,2008,34(03):58-62.
Geng Wenzhong.Tentative design of starting test system for new liquid rocket engine test bed[J].Journal of Rocket Propulsion,2008,34(03):58-62.
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Geng Wenzhong.Tentative design of starting test system for new liquid rocket engine test bed[J].Journal of Rocket Propulsion,2008,34(03):58-62.
新型液体火箭发动机试车台 起动试验系统方案设计
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
34
期数:
2008年03期
页码:
58-62
栏目:
燃料与推进剂
出版日期:
2008-06-30
- Title:
- Tentative design of starting test system for new liquid rocket engine test bed
- Keywords:
- test bed; engine starting test; tentative design
- 分类号:
- V434
- 文献标志码:
- A
- 摘要:
- 为满足总体对发动机地面试验入口压力的设计要求，提出了三种试车台起动试 验系统设计方案。论证表明，设计方案可行，布局紧凑、合理。综合考虑，确定起动容器与 主容器接力试验系统作为新建台的设计方案。
- Abstract:
- To meet the engine ground test inlet pressure design requirements of the generM pro— posal and the design task document．Three tentative designs of starting test system of the test bed were proposed and their feasibilities were proved．Upon the construction document of the new test bed，the optimum design of starting tank with the combination of compact layout and the reasonable structure design was stated in this paper．The new design of starting test system of the test bed meets the general design proposal requirements on the engine ground starting test，and provides the experi· ence for the future test bed building．
参考文献/References:
[l]曾源华，张政．液体火箭发动机试验[M]．宇航出版社，1990．
[2]机械工程手册[M]．机械工业出版社，1982，(2)．
[3]马瀚英．访苏考察纪要[J]．国外航天推进试验技术．199Z
(2)：6-9．
[4]夏兆熊．两德和意大利火箭发动机地面试验技术介绍[J]．
国外航天推进试验技术．1992，(1)：20—29．
[5]李伟民．液氧／煤油发动机试验起动过程推进剂供应技
术[J]．火箭推进。2006。32(3)：56—62．
[6]程磊．液氧／煤油发动机换热器试车台配气系统设计[J]．
火箭推进．2006，32(5)：60—62．
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备注/Memo
收稿日期：2007—09—27；修回日期：2008-02—13。 作者简介：耿文忠(1950-)，男，高级T程师．研究领域为液体火箭发动机试验技术。
更新日期/Last Update:
1900-01-01