Influential Analysis of Parameters Variation of Propulsion System on Longitudinal Vibration Response in Liquid Rockets

Tang Ye 1 Fang Bo 1 Zhang Yewei 2, 3 Tan Lijun1 Yu Ziwen 4

Journal of Vibration and Shock ›› 2015, Vol. 34 ›› Issue (12) : 189-194.

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Journal of Vibration and Shock ›› 2015, Vol. 34 ›› Issue (12) : 189-194.

Influential Analysis of Parameters Variation of Propulsion System on Longitudinal Vibration Response in Liquid Rockets

  • Tang Ye 1   Fang Bo 1    Zhang Yewei 2, 3  Tan Lijun1  Yu Ziwen 4 
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Abstract

 To optimize the propulsion system in liquid rockets, avoid the low frequency vibration environment deterioration of liquid rockets which is caused by POGO vibration has disadvantage effect on the flight course of rocket system, the dynamic model of POGO vibration system in liquid rockets is established, the model of sensitivity analysis that longitudinal vibration response in liquid rockets (LVRILR) with respect to parameters of propulsion system is proposed in the time domain based on the dynamic sensitivity technique. Through numerical calculation, the laws that the inertial parameters variation of fluid, the drag parameters variation of fluid, the stiffness parameters variation of fluid and the dynamic gain variation of pump for propulsion system have an important effect on LVRILR are obtained. The results obtained show the sensitive extent of LVRILR with respect to the inertial parameters of fluid and the drag parameters of fluid is sharply greater than the stiffness parameters of fluid, the influence that the dynamic gain variation of pump has on LVRILR is the maximum, and the influence that the variation of fluid stiffness for the short pipeline which is on pump front has on LVRILR is the minimum. This provides a reference for longitudinal vibration in liquid rockets is reduced and the characteristics of POGO vibration are further researched. 
 

Key words

liquid rockets / POGO vibration / longitudinal vibration response / parameters of propulsion system / sensitivity

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Tang Ye 1 Fang Bo 1 Zhang Yewei 2, 3 Tan Lijun1 Yu Ziwen 4 . Influential Analysis of Parameters Variation of Propulsion System on Longitudinal Vibration Response in Liquid Rockets[J]. Journal of Vibration and Shock, 2015, 34(12): 189-194

References

[1] Rubin S. Longitudinal instability of liquid rockets due to propulsion feedback (POGO)[J]. Journal of Spacecraft and Rockets, 1966, 3(8): 1188-1195.
[2] Nagai H, Noda K, Yamazaki I, Mori T. Status of H-Ⅱ rocket first stage propulsion system[J]. Journal of Propulsion and Power, 1992, 8(2): 313-319.
[3] Meyers J F. Delta Ⅱ-A new generation begins[J]. AIAA Journal, 1989, 89-2740:1-10.
[4] 黄怀德.液体火箭的POGO振动研究[J].振动工程学报,1987, 1(1): 5-13.
    Huang Huaide. Research into POGO vibration of liquid rockets[J]. Journal of Vibration Engineering, 1987, 1(1): 5-13.
[5] Ujino T. POGO Prevention of H-2 launch vehicle[J]. AIAA Journal, 1994, 94-1624-CP: 2858-2867.
[6] Lack M H, Rubin S. Passive suppression of POGO on the space shuttle[R].NASA CR-132452, 1974.
[7] Marius T J. Investigation on active suppression of POGO[J]. AIAA Journal, 1995, 1995-3311-CP: 1239-1249.
[8] Zhao Z H, Ren G X, Yu Z W, et al. Parameter study on POGO stability of liquid rockets[J].Journal of Spacecraft and Rockets,2011,48(3):537-541.
[9] Dotson K W, Rubin S, Sako B H. Mission-specific POGO stability analysis with correlated pump parameters[J]. Journal of Propulsion and Power, 2005, 21:619-626
[10] Muller S, Breviere F, Kemilis A ,et al. Influence pump cavitation process on POGO diagnosis for the A5E/CA upper stage[J].AIAA Journal, 2010, 2010-6892:1-18.
[11] Ryan R S, Kiefling A K, Buchanan H J, et al. Simulation of Saturn V S-Ⅱ stage propellant feedline dynamics[J].Journal of Spacecraft and Rockets, 1970, 7(12): 1407-1412.
[12]  Choi K M, Jo H K, Kim W H, et al. Sensitivity analysis of non-conservative eigensystems[J].Journal of Sound and Vibration, 2004,271:997-1011.
[13]  黄益民,刘伟,刘永寿等.充液管道模态的参数灵敏度及其共振可靠性分析[J]. 振动与冲击, 2010, 29(1): 193-196
 Huang Yimin,Liu Wei,Liu Yongshou,et al.Parameter sensitivity and resonance reliability of a fluid-filled pipeline[J].Journal of Vibration and Shock,2010, 29(1): 193-196.
[14] Zhang Yimin, Huang Xianzhen, Zhao Qun. Sensitivity analysis for vibration transfer path systems with non-viscous damping[J].Journal of Vibration and Control, 2011, 17(7): 1042-1048.
[15] Oppenheinm B W, Rubin S. Advanced POGO stability analysis for liquid rockets[J].Journal of Spacecraft and Rockets, 1993.30(3): 360-373.
[16] 王其政,黄怀德,姚德源.结构耦合动力学[M].北京:宇航出版社,1999:251-273.
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