| CK－lM无人机双发助推试验研究 |
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| 引用本文： | 施允涛. CK－lM无人机双发助推试验研究[J]. 航空学报, 1994, 15(7): 866-869 |
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| 作者姓名： | 施允涛 |
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| 作者单位： | 南京航空航天大学447信箱,南京,210016 |
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| 摘 要： | 论述了ＣＫ－１型无人机闭锁力的确定、双发助推器的同步性及其投放特性,经试飞表明,闭锁力确定合理,双发助推器同步性良好,投放安全。
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| 关 键 词： | 无人飞机 锁－力 助推火箭发动机 同步 |
| 收稿时间： | 1993-03-02 |
| 修稿时间： | 1993-09-26 |
A STUDY OF THk CK-lM PILOTLESS AIRCRAFT WITH TWO BOOSTERS |
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| Shi Yuntao. A STUDY OF THk CK-lM PILOTLESS AIRCRAFT WITH TWO BOOSTERS[J]. Acta Aeronautica et Astronautica Sinica, 1994, 15(7): 866-869 |
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| Authors: | Shi Yuntao |
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| Affiliation: | P. O. Box. 447 of Nanijing University of Aeronautics and Astronautics,Nanjing,210016 |
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| Abstract: | The detennination of locking force and the synchronism and drop of two boosters on CK-lM pilotless aircraft are studied.The fiight tests verify that the locking force is suitable,the synchronism of the CK-lM pilotless aircraft with two boosters is good,and the drop of boosters is safe. |
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| Keywords: | pilotless aircraft locks(fastener)forces booster rocket engine synchronism |
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