Dynamic-Envelope Analysis of Clamp-Band Joint Considering Pyroshock of Satellite Separation-Reference-Cited by-同舟云学术

Dynamic-Envelope Analysis of Clamp-Band Joint Considering Pyroshock of Satellite Separation

Published:2014-09 Issue:5 Volume:51 Page:1390-1400
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Li Junlan¹,Yan Shaoze²,Tan Xuefeng²

Affiliation:

1. School of Mechanical Engineering, Key Laboratory of Mechanism Theory and Equipment Design of the Ministry of Education, Tianjin University, 300072 Tianjin, People’s Republic of China

2. Department of Mechanical Engineering, State Key Laboratory of Tribology, Tsinghua University, 100084 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A32382

Reference24 articles.

1. Rigid body separation dynamics for space launch vehicles

2. CONING EFFECTS CAUSED BY SEPARATION OF SPIN-STABILIZED STAGES

3. Comment on "Coning Effects Caused by Separation of Spin-Stabilized Stages"

4. Stage separation dynamics of spin-stabilized rockets

5. Stage separation of parallel-staged shuttle vehicles - A capability assessment.

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