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Thermally induced vibration of composite solar array with honeycomb panels in low earth orbit

  • Published:2014-10 Issue:1 Volume:71 Page:419-432
  • ISSN:1359-4311
  • Container-title:Applied Thermal Engineering
  • language:en
  • Short-container-title:Applied Thermal Engineering

Author:

Li JunlanORCID,Yan Shaoze

Funder

National Natural Science Foundation of China

National High Technology Research and Development Program of China

Key Laboratory of Mechanism Theory and Equipment Design of the Ministry of Education

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference28 articles.

1. Preserving mission, on-orbit modifications to Hubble space telescope pointing control system;Nurre;J. Guid. Control Dyn.,1995

2. Solar-array-induced disturbance of hubble space telescope pointing system;Foster;J. Spacecr. Rockets,1995

3. Airclaims Ascend SpaceTrak Database,2010

4. Reliability analysis method of a solar array by using fault tree analysis and fuzzy reasoning Petri net;Wu;Acta Astronaut.,2011

5. Dynamic response of rapidly heated space structure;Thornton,1992

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