Volume 44 Issue 4
Apr.  2018
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ZHANG Taihua, JIANG Luhua, ZHOU Jianghuaet al. Kinematic and mechanical analysis on launch process of stratospheric airship[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(4): 691-699. doi: 10.13700/j.bh.1001-5965.2017.0227(in Chinese)
Citation: ZHANG Taihua, JIANG Luhua, ZHOU Jianghuaet al. Kinematic and mechanical analysis on launch process of stratospheric airship[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(4): 691-699. doi: 10.13700/j.bh.1001-5965.2017.0227(in Chinese)

Kinematic and mechanical analysis on launch process of stratospheric airship

doi: 10.13700/j.bh.1001-5965.2017.0227
Funds:

National High-tech Research and Development Program of China 2013AA122904

National Science and Technology Major Project 

More Information
  • Corresponding author: JIANG Luhua, E-mail: jianglh@ihep.ac.cn
  • Received Date: 13 Apr 2017
  • Accepted Date: 22 May 2017
  • Publish Date: 20 Apr 2018
  • Launch mode of the stratospheric airship is the prerequisite factor to safely reach the target altitude. In this paper, a dynamics model for the launch process of stratospheric airship is firstly established, and the analytical solution method is put forward, and the quantitative analysis is carried out. Secondly, according to the typical issues that influence the launch process, the dynamic analysis of both the single-helium and multi-helium envelope structure are carried out, including dynamics response and force status. Furthermore, the numerical results of a single helium envelope structure are obtained and then compared with experimental data. The result verified the accuracy of the analytical method, which can also provide the basis for launch process of the airship and the design of the launch equipment.

     

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