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Solubilities of CO(2), O(2) and N(2) in rocket propellant 5 under low pressure

The static method of isochoric saturation was used to measure the solubilities of CO(2), O(2) and N(2) in rocket propellant 5 (RP5) at temperatures ranging from 253.15 to 323.15 K in 10 K intervals and pressures ranging from 0 to 120 kPa. The measurement accuracy of the constructed experimental setu...

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Autores principales: Li, Chaoyue, Feng, Shiyu, Xu, Lei, Peng, Xiaotian, Liu, Weihua
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Nature Publishing Group UK 2022
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8927475/
https://www.ncbi.nlm.nih.gov/pubmed/35296706
http://dx.doi.org/10.1038/s41598-022-08340-8
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author Li, Chaoyue
Feng, Shiyu
Xu, Lei
Peng, Xiaotian
Liu, Weihua
author_facet Li, Chaoyue
Feng, Shiyu
Xu, Lei
Peng, Xiaotian
Liu, Weihua
author_sort Li, Chaoyue
collection PubMed
description The static method of isochoric saturation was used to measure the solubilities of CO(2), O(2) and N(2) in rocket propellant 5 (RP5) at temperatures ranging from 253.15 to 323.15 K in 10 K intervals and pressures ranging from 0 to 120 kPa. The measurement accuracy of the constructed experimental setup was verified by measuring the solubility of CO(2) in water. The relative expanded uncertainty (k = 2) in the solubility data was less than 4.0%. The solubilities of CO(2), O(2) and N(2) in RP5 increased with pressure. As the temperature increased, the solubility decreased for CO(2) solubility and increased for O(2) and N(2). Henry's constants for the three gases in RP5 decreased over the experimental temperature and pressure ranges in the order of N(2) > O(2) > CO(2). The measured solubilities of CO(2), O(2) and N(2) could be fitted with a modified Krichevsky–Kasarnovsky equation, and the maximum deviation between the measured and calculated data was less than 8.04%, 7.03% and 6.18%, respectively.
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spelling pubmed-89274752022-03-17 Solubilities of CO(2), O(2) and N(2) in rocket propellant 5 under low pressure Li, Chaoyue Feng, Shiyu Xu, Lei Peng, Xiaotian Liu, Weihua Sci Rep Article The static method of isochoric saturation was used to measure the solubilities of CO(2), O(2) and N(2) in rocket propellant 5 (RP5) at temperatures ranging from 253.15 to 323.15 K in 10 K intervals and pressures ranging from 0 to 120 kPa. The measurement accuracy of the constructed experimental setup was verified by measuring the solubility of CO(2) in water. The relative expanded uncertainty (k = 2) in the solubility data was less than 4.0%. The solubilities of CO(2), O(2) and N(2) in RP5 increased with pressure. As the temperature increased, the solubility decreased for CO(2) solubility and increased for O(2) and N(2). Henry's constants for the three gases in RP5 decreased over the experimental temperature and pressure ranges in the order of N(2) > O(2) > CO(2). The measured solubilities of CO(2), O(2) and N(2) could be fitted with a modified Krichevsky–Kasarnovsky equation, and the maximum deviation between the measured and calculated data was less than 8.04%, 7.03% and 6.18%, respectively. Nature Publishing Group UK 2022-03-16 /pmc/articles/PMC8927475/ /pubmed/35296706 http://dx.doi.org/10.1038/s41598-022-08340-8 Text en © The Author(s) 2022 https://creativecommons.org/licenses/by/4.0/Open Access This article is licensed under a Creative Commons Attribution 4.0 International License, which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons licence, and indicate if changes were made. The images or other third party material in this article are included in the article's Creative Commons licence, unless indicated otherwise in a credit line to the material. If material is not included in the article's Creative Commons licence and your intended use is not permitted by statutory regulation or exceeds the permitted use, you will need to obtain permission directly from the copyright holder. To view a copy of this licence, visit http://creativecommons.org/licenses/by/4.0/ (https://creativecommons.org/licenses/by/4.0/) .
spellingShingle Article
Li, Chaoyue
Feng, Shiyu
Xu, Lei
Peng, Xiaotian
Liu, Weihua
Solubilities of CO(2), O(2) and N(2) in rocket propellant 5 under low pressure
title Solubilities of CO(2), O(2) and N(2) in rocket propellant 5 under low pressure
title_full Solubilities of CO(2), O(2) and N(2) in rocket propellant 5 under low pressure
title_fullStr Solubilities of CO(2), O(2) and N(2) in rocket propellant 5 under low pressure
title_full_unstemmed Solubilities of CO(2), O(2) and N(2) in rocket propellant 5 under low pressure
title_short Solubilities of CO(2), O(2) and N(2) in rocket propellant 5 under low pressure
title_sort solubilities of co(2), o(2) and n(2) in rocket propellant 5 under low pressure
topic Article
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8927475/
https://www.ncbi.nlm.nih.gov/pubmed/35296706
http://dx.doi.org/10.1038/s41598-022-08340-8
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