https://www.scipedia.com/wd/index.php?action=history&feed=atom&title=Youhuan_et_al_2015aYouhuan et al 2015a - Revision history2026-04-17T07:58:25ZRevision history for this page on the wikiMediaWiki 1.27.0-wmf.10https://www.scipedia.com/wd/index.php?title=Youhuan_et_al_2015a&diff=202399&oldid=prevScipediacontent: Scipediacontent moved page Draft Content 231727507 to Youhuan et al 2015a2021-02-02T05:47:53Z<p>Scipediacontent moved page <a href="/public/Draft_Content_231727507" class="mw-redirect" title="Draft Content 231727507">Draft Content 231727507</a> to <a href="/public/Youhuan_et_al_2015a" title="Youhuan et al 2015a">Youhuan et al 2015a</a></p>
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</td></tr></table>Scipediacontenthttps://www.scipedia.com/wd/index.php?title=Youhuan_et_al_2015a&diff=202398&oldid=prevScipediacontent: Created page with " == 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 accu..."2021-02-02T05:47:48Z<p>Created page with " == 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 accu..."</p>
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== Abstract ==<br />
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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.<br />
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== Original document ==<br />
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The different versions of the original document can be found in:<br />
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* [http://dx.doi.org/10.5220/0005505801810187 http://dx.doi.org/10.5220/0005505801810187]<br />
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* [https://doi.org/10.5220/0005505801810187 https://doi.org/10.5220/0005505801810187] under the license cc-by-nc-nd<br />
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* [https://dblp.uni-trier.de/db/conf/icinco/icinco2015-2.html#XiangZLC15 https://dblp.uni-trier.de/db/conf/icinco/icinco2015-2.html#XiangZLC15],<br />
: [https://academic.microsoft.com/#/detail/2310979030 https://academic.microsoft.com/#/detail/2310979030]</div>Scipediacontent