Filling Accuracy Analysis of the Rocket Propellant based on the Flowmeter Measuring Model

Xiang Youhuan, Zhang Ping, Liu Weidong, Cui Benting

Abstract

The high filling accuracy of rocket propellant is an important guarantee for the success of the rocket launch. In view of the factors that affect filling accuracy of the rocket propellant in the filling system of the spaceflight launch site, the algorithm of propellant filling accuracy calculation based on the flowmeter measuring model is proposed in this paper. It respectively carries through mathematical analyses for the different factors affecting the filling accuracy. Through the proposed algorithm, numerical calculation has been carried on the comprehensive filling accuracy of rocket propellant under the existing filling process. It can provide theoretical basis and data support for optimizing filling control process and improving filling accuracy in the launch site, so as to further improving the success rate of rocket launch.

References

  1. Deng Y, Qin G, Wang M, et al. Study on performance degradation simulation and evaluation method for pneumatic ball valve of Propellant Filling System[C]. Quality, Reliability, Risk, Maintenance, and Safety Engineering (ICQR2MSE), 2012 International Conference on. IEEE, 2012: 144-147.
  2. Zhuang Ke. Design and implementation of the conventional propellant filling factor range application system. National University of Defense Technology, 2005.
  3. Xiang Youhuan, Shi Jinfeng, Li Liqun, et al. Accuracy Analysis on Measuring Model of Rocket Propellant Filling Based on Weight Measurement[C]. IEEE International Conference ICSPCC2014, 2014.8: 281-286.
  4. Ma Jian, Tong Fei, Chen Zu-kui. Analysis on deviation and measuring precision of tank volume[J]. Journal of Rocket Propulsion. 2013 (1): 41-45.
  5. Yang Zhi-qiang, Zhang Hong-jian, Huang Yong-mei. Research on data value simulation of fluid field characteristic of vortex flowmeter[J]. Process Automation Instrumentation. 2004, 25(5):10-13.
  6. Yan Xiao-qing, Li Zi-ran, Zhou Jin. Calculation of bookbinding parameters and integrating method of the software of liquid propellant utilizing system. Jourmal of National University of Defense Technology. 2004, 26(6): 79-81.
  7. Pan Yong-cheng, Wang Yong, Xie Yu-dong. Analysis of Inner Flow Field Characteristics of a Control Valve Based on CFD[J]. Machine Tool & Hydraulics. Vol.39 No.1 Jan.2011:5-7.
  8. Ma Xiaolin, Chen Guoding. Dynamics and Leakage Analysis of Padded Finger Seal Based on Equivalent Model[J]. Acta Aeronautica et Astronautica Sinica. Vol.29 No.5 Sept.2008:1356-1363.
  9. Dong Yu-hua, Zhou Jing-en. Numerical Calculation of Gas Leakage Rate in the Long-transport Pipeline. Oil & Gas Storage and Transportation. Vol.21 No.8 2002:11-15.
  10. Zou W, Yu K, Wan X. Research on the gas-leakage rate of unsteady ventilated supercavity[J]. Journal of Hydrodynamics, Ser. B, 2010, 22(5): 778-783.
  11. Beirami M K, Nabavi S V, Chamani M R. Free overfall in channels with different cross sections and sub-critical flow[J]. Iranian Journal of Science & Technology, Transaction B, Engineering, 2006, 30(B1).
  12. Boonen E, Van Puyvelde P, Moldenaers P. Droplet dynamics in sub-critical complex flows[J]. Rheologica acta, 2009, 48(4): 359-371.
  13. Cazauran X, Birembaut Y, Hahn R, et al. Gas Leakage Correlation[C]//ASME 2009 Pressure Vessels and Piping Conference. American Society of Mechanical Engineers, 2009: 243-249.
  14. Zhang S, Liu W, Zhang Y, et al. Gas leakage monitoring with scanned-wavelength direct absorption spectroscopy[J]. Chinese Optics Letters, 2010, 8(5): 443-446.
  15. Ben-Mansour R, Habib M A, Khalifa A, et al. Computational fluid dynamic simulation of small leaks in water pipelines for direct leak pressure transduction[J]. Computers & Fluids, 2012, 57: 110-123.
Download


Paper Citation


in Harvard Style

Youhuan X., Ping Z., Weidong L. and Benting C. (2015). Filling Accuracy Analysis of the Rocket Propellant based on the Flowmeter Measuring Model . In Proceedings of the 12th International Conference on Informatics in Control, Automation and Robotics - Volume 2: ICINCO, ISBN 978-989-758-123-6, pages 181-187. DOI: 10.5220/0005505801810187


in Bibtex Style

@conference{icinco15,
author={Xiang Youhuan and Zhang Ping and Liu Weidong and Cui Benting},
title={Filling Accuracy Analysis of the Rocket Propellant based on the Flowmeter Measuring Model},
booktitle={Proceedings of the 12th International Conference on Informatics in Control, Automation and Robotics - Volume 2: ICINCO,},
year={2015},
pages={181-187},
publisher={SciTePress},
organization={INSTICC},
doi={10.5220/0005505801810187},
isbn={978-989-758-123-6},
}


in EndNote Style

TY - CONF
JO - Proceedings of the 12th International Conference on Informatics in Control, Automation and Robotics - Volume 2: ICINCO,
TI - Filling Accuracy Analysis of the Rocket Propellant based on the Flowmeter Measuring Model
SN - 978-989-758-123-6
AU - Youhuan X.
AU - Ping Z.
AU - Weidong L.
AU - Benting C.
PY - 2015
SP - 181
EP - 187
DO - 10.5220/0005505801810187