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

Xiang Youhuan, Zhang Ping, Liu Weidong, Cui Benting

2015

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.

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