Study on Line Sail in the Process of Double-guided Parachute Deployment

被引：1
作者：
Zhang, Mingliang [1 ]
Gao, Puyun [1 ]
机构：
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Hunan, Peoples R China
来源：
2019 5TH INTERNATIONAL CONFERENCE ON ENERGY MATERIALS AND ENVIRONMENT ENGINEERING | 2019年 / 295卷
关键词：
D O I：
10.1088/1755-1315/295/4/042101
中图分类号：
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号：
0807 ; 0820 ;
摘要：
Double-guided deceleration parachute is widely used in large-scale space return activities. Compared with single-guided parachute, it has higher security, but its structure is more complex. This paper aims to study on line sail and analyse the effects of different initial dynamic pressure, separation speeds and angles of attack on the phenomenon during double-guided parachute deployment. The results show that for the double-guided parachute, the bigger the dynamic pressure of the return cabin is, the smaller the separation speed is, the bigger the angle of attack is, the more serious the line sail phenomenon will be.
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页数：5
相关论文
共 15 条
  • [1] Guo Peng, 2012, RES OPENING PROCESS
  • [2] [鲁媛媛 Lu Yuanyuan], 2014, [宇航学报, Journal of Astronautics], V35, P1238
  • [3] Mcvey D F, 1974, AIRCRAFT, V11, P96
  • [4] Mitcheltree R, AM I AERONAUTICS AST, V16, P59
  • [5] Moog R D, 751381 AIAA
  • [6] PURVIS J, 1984, 8 AIAA AER DEC BALL
  • [7] PURVIS J W, 1984, PARACHUTES
  • [8] PURVIS J W, 2013, AIAA J
  • [9] Song Xumin, 2009, SPACECR REC REM SENS, V30, P16
  • [10] Wang Hai-tao, 2010, Journal of National University of Defense Technology, V32, P49
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