Structural Modeling Reflected Nonlinearity for Longitudinal Dynamic Instability (POGO) Analysis of Liquid Propellant Launch Vehicles in Preliminary Design Phase-Reference-Cited by-同舟云学术

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Structural Modeling Reflected Nonlinearity for Longitudinal Dynamic Instability (POGO) Analysis of Liquid Propellant Launch Vehicles in Preliminary Design Phase

Published:2015-08-28 Issue: Volume: Page:
ISSN:
Container-title:AIAA SPACE 2015 Conference and Exposition
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Author:

Kim Junbeom¹,Shin Sang Joon¹,Park Jongho¹,Kim Youdan¹

Affiliation:

1. Seoul National University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-4594

Reference27 articles.

1. Longitudinal instability of liquid rockets due to propulsion feedback /POGO/.

2. Advanced Pogo stability analysis for liquid rockets

3. 4Anonymous, "NASA Space Vehicle Design Criteria - Prevention of Coupled Structure-Propulsion Instability (POGO)," NASASP-8055,1970.

4. 5Anonymous, "NASASpaceVehicleDesign Criteria- Natural VibrationModal Analysis,"NASASP-8012, 1970.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Integrated one-dimensional dynamic analysis methodology for space launch vehicles reflecting liquid components;The Aeronautical Journal;2017-07-11

2. Further Extended Structural Modeling and Modal Analysis of Liquid Propellant Launch Vehicles for Pogo Analysis;AIAA SPACE 2016;2016-09-09

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