航空学报 > 1994, Vol. 15 Issue (7): 866-869

CK-lM无人机双发助推试验研究

施允涛   

  1. 南京航空航天大学447信箱,南京,210016
  • 收稿日期:1993-03-02 修回日期:1993-09-26 出版日期:1994-07-25 发布日期:1994-07-25

A STUDY OF THk CK-lM PILOTLESS AIRCRAFT WITH TWO BOOSTERS

Shi Yuntao   

  1. P. O. Box. 447 of Nanijing University of Aeronautics and Astronautics,Nanjing,210016
  • Received:1993-03-02 Revised:1993-09-26 Online:1994-07-25 Published:1994-07-25

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。

关键词: 无人飞机, 锁-力, 助推火箭发动机, 同步

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.

Key words: pilotless aircraft, locks(fastener)-forces, booster rocket engine, synchronism

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