| 引用本文: | 肖翠蓉.761 探空火箭喷管绝热内衬的工艺探讨.[J].国防科技大学学报,1982,(1):117-137.[点击复制] |
| Xiao Cuirong.Study of the Technological Process of Adiabatic Bush for《761》Sounding Rocket Nozzle[J].Journal of National University of Defense Technology,1982,(1):117-137[点击复制] |
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| 761 探空火箭喷管绝热内衬的工艺探讨 |
| 肖翠蓉 |
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| 摘要: |
| 本文通过对761探空火箭喷管绝热内衬的研制，叙述了该绝热内衬的选材和结构的确定。重点讨论了用模压法压制绝热内衬中，一些主要工艺参数的选择。
文中通过大量试验数据，说明了该绝热内衬的结构合理，工艺简便，工作可靠，适宜于作761探空火箭喷管绝热件之用 ，并可推荐到其它兵器作绝热内衬使用。 |
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| 投稿日期：1981-09-14 |
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| Study of the Technological Process of Adiabatic Bush for《761》Sounding Rocket Nozzle |
| Xiao Cuirong |
| Abstract: |
| This report describes the selection of materials and the determination of structure about adiabatic bush used for《761》sounding rocket nozzle. Particularly，the selection of some main technological paramenters is discussed when the adiabatie bush is made by compression molding method. A great number of testing data prove that the structure of adiabatic bush is reasonable，the technological process is convenient，operation is reliable，so that，it can be used for adiabatic bush in《761》sounding rocket nozzle and other weapons. |
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