Thermal Decomposition, Ignition Process and Combustion Behavior of Nitrate Ester Plasticized Polyether Propellant at 0.1–3.0 MPa
Nitrate ester plasticized polyether (NEPE) propellant is widely used in solid rocket motors, having both good mechanical properties and high specific impulse. However, its ignition and combustion process are complex and need to be better understood. In this study, a high-pressure sealed combustion c...
Saved in:
Published in | International journal of aerospace engineering Vol. 2022; pp. 1 - 12 |
---|---|
Main Authors | , , , , , , , |
Format | Journal Article |
Language | English |
Published |
New York
Hindawi
2022
Hindawi Limited Wiley |
Subjects | |
Online Access | Get full text |
Cover
Loading…
Abstract | Nitrate ester plasticized polyether (NEPE) propellant is widely used in solid rocket motors, having both good mechanical properties and high specific impulse. However, its ignition and combustion process are complex and need to be better understood. In this study, a high-pressure sealed combustion chamber was constructed, a thermogravimetry-differential scanning calorimetry was used to investigate the thermal decomposition process, and a high-speed camera was used to capture the ignition process and combustion behavior of the propellant. The results showed that the thermal decomposition process of this propellant could be divided into two stages. The first stage (50–350°C) was the major mass loss stage and exhibited typical features of BTTN, RDX, and AP decomposition. The second stage (350–500°C) was mainly accompanied by decomposition of the remaining components as well as slight oxidation of aluminum particles. The ignition process of NEPE propellant was divided into four stages, including the inert heating period stage, thermal decomposition stage, initial flame stage, and stable combustion stage. After the propellant absorbed heat, the propellant started to pyrolyze and gasify to generate flammable gas. When the temperature of the propellant surface reached the flammable gas ignition point, an initial flame was generated on the surface, which spread rapidly, covering the surface. The ignition delay time of the propellant was measured by a signal acquisition system, and a mathematical model was then established for the ignition delay time. The results showed that the ignition delay time decreased with increased laser heat flux and ambient pressure. Finally, the Vielle burning rate empirical formula was used to fit the burning rate data for the propellant. The resulting good fit was consistent with experimental measurements and showed that the formula was valid for predicting the NEPE propellant burning rate under 0.1–3.0 MPa nitrogen. |
---|---|
AbstractList | Nitrate ester plasticized polyether (NEPE) propellant is widely used in solid rocket motors, having both good mechanical properties and high specific impulse. However, its ignition and combustion process are complex and need to be better understood. In this study, a high-pressure sealed combustion chamber was constructed, a thermogravimetry-differential scanning calorimetry was used to investigate the thermal decomposition process, and a high-speed camera was used to capture the ignition process and combustion behavior of the propellant. The results showed that the thermal decomposition process of this propellant could be divided into two stages. The first stage (50–350°C) was the major mass loss stage and exhibited typical features of BTTN, RDX, and AP decomposition. The second stage (350–500°C) was mainly accompanied by decomposition of the remaining components as well as slight oxidation of aluminum particles. The ignition process of NEPE propellant was divided into four stages, including the inert heating period stage, thermal decomposition stage, initial flame stage, and stable combustion stage. After the propellant absorbed heat, the propellant started to pyrolyze and gasify to generate flammable gas. When the temperature of the propellant surface reached the flammable gas ignition point, an initial flame was generated on the surface, which spread rapidly, covering the surface. The ignition delay time of the propellant was measured by a signal acquisition system, and a mathematical model was then established for the ignition delay time. The results showed that the ignition delay time decreased with increased laser heat flux and ambient pressure. Finally, the Vielle burning rate empirical formula was used to fit the burning rate data for the propellant. The resulting good fit was consistent with experimental measurements and showed that the formula was valid for predicting the NEPE propellant burning rate under 0.1–3.0 MPa nitrogen. |
Author | Li, Weixuan Feng, Yaya Tu, Chengyin Zhou, Changsheng Ling, Zhigang Li, Yingkun Cai, Wenxiang Chen, Xiong |
Author_xml | – sequence: 1 givenname: Chengyin surname: Tu fullname: Tu, Chengyin organization: School of Mechanical EngineeringNanjing University of Science and TechnologyNanjing 210094Chinanjust.edu.cn – sequence: 2 givenname: Yaya surname: Feng fullname: Feng, Yaya organization: The Synthetic Chemical and Engineering Institute of Inner MongoliaHohhot 010010China – sequence: 3 givenname: Zhigang surname: Ling fullname: Ling, Zhigang organization: The Synthetic Chemical and Engineering Institute of Inner MongoliaHohhot 010010China – sequence: 4 givenname: Xiong orcidid: 0000-0002-8854-5720 surname: Chen fullname: Chen, Xiong organization: School of Mechanical EngineeringNanjing University of Science and TechnologyNanjing 210094Chinanjust.edu.cn – sequence: 5 givenname: Changsheng surname: Zhou fullname: Zhou, Changsheng organization: School of Mechanical EngineeringNanjing University of Science and TechnologyNanjing 210094Chinanjust.edu.cn – sequence: 6 givenname: Yingkun orcidid: 0000-0002-1483-9101 surname: Li fullname: Li, Yingkun organization: School of Mechanical EngineeringNanjing University of Science and TechnologyNanjing 210094Chinanjust.edu.cn – sequence: 7 givenname: Weixuan surname: Li fullname: Li, Weixuan organization: School of Mechanical EngineeringNanjing University of Science and TechnologyNanjing 210094Chinanjust.edu.cn – sequence: 8 givenname: Wenxiang surname: Cai fullname: Cai, Wenxiang organization: School of Mechanical EngineeringNanjing University of Science and TechnologyNanjing 210094Chinanjust.edu.cn |
BookMark | eNp9kb1uGzEQhInABvzb-QEIpIxl847k8Vgmsp0I8I8Kuyb2eHsWhdNRIakEduUiTeq8oZ8klGS4dLWL2Q-zA8wB2Rn8gIScFOysKKQ8L1lZnleCa1WrT2S_qGo1klqJnfe9qvbIQYxzxiomldwnf-5nGBbQ0wu0frH00SXnh1M6eRw2G50GbzFGCkNLx37RrOJG_oYz-OV8oL6jty4FSEgvY8JApz1kxLpnbOnU90-YZms1-CX2PQyJQqI57-vLP37GXl_-3kzhiOx20Ec8fpuH5OHq8n78Y3R9930y_no9soLxNFJK27LiCIyJTkotC6saVkvBmWWy4bbuJDayEDwfmxY46K7U3ErbVFpZ5IdksvVtPczNMrgFhCfjwZmN4MOjgZCz92gE2lqgbG2NKGrdgEXFtO5Ey8CWXGSvz1uvZfA_VxiTmftVGHJ8U6ocV-qCyUydbikbfIwBu_evBTPrzsy6M_PWWca_bPGZG1r47T6m_wPo4ZnM |
CitedBy_id | crossref_primary_10_1016_j_combustflame_2024_113500 |
Cites_doi | 10.2514/3.3011 10.1016/S0010-2180(01)00281-4 10.1016/j.combustflame.2011.06.020 10.1615/IntJEnergeticMaterialsChemProp.2013005557 10.4028/www.scientific.net/AMR.549.1037 10.1007/s10973-020-09297-4 10.1002/prep.201500080 10.1016/j.combustflame.2013.02.019 10.1002/prep.201700059 10.1002/cjoc.201090132 10.1002/prep.201700191 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.300 10.1002/prep.201600131 10.2514/3.51071 10.1016/j.tca.2015.04.025 10.1080/00102200302358 10.2514/3.3213 10.1002/prep.200500025 10.1080/00102207308946646 10.1016/j.dt.2022.05.016 10.1016/j.jhazmat.2017.08.055 10.1002/prep.202000170 10.1016/S0082-0784(71)80105-4 10.1023/A:1017561827203 10.1155/2020/8858057 10.1080/00102202.2018.1460599 10.1002/prep.202000326 10.1080/00102207508946677 10.1016/0010-2180(79)90008-7 10.1002/prep.201600291 10.3390/molecules25102276 10.13224/j.cnki.jasp.20220229 10.1016/j.dt.2020.09.020 10.2514/1.36458 |
ContentType | Journal Article |
Copyright | Copyright © 2022 Chengyin Tu et al. Copyright © 2022 Chengyin Tu et al. This is an open access article distributed under the Creative Commons Attribution License (the “License”), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License. https://creativecommons.org/licenses/by/4.0 |
Copyright_xml | – notice: Copyright © 2022 Chengyin Tu et al. – notice: Copyright © 2022 Chengyin Tu et al. This is an open access article distributed under the Creative Commons Attribution License (the “License”), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License. https://creativecommons.org/licenses/by/4.0 |
DBID | RHU RHW RHX AAYXX CITATION 7TB 8FD 8FE 8FG ABJCF ABUWG AFKRA ARAPS AZQEC BENPR BGLVJ CCPQU CWDGH DWQXO FR3 H8D HCIFZ L6V L7M M7S P5Z P62 PIMPY PQEST PQQKQ PQUKI PRINS PTHSS DOA |
DOI | 10.1155/2022/6439787 |
DatabaseName | Hindawi Publishing Complete Hindawi Publishing Subscription Journals Open Access Journals (Hindawi Publishing) CrossRef Mechanical & Transportation Engineering Abstracts Technology Research Database ProQuest SciTech Collection ProQuest Technology Collection Materials Science & Engineering Collection ProQuest Central (Alumni) ProQuest Central Advanced Technologies & Aerospace Collection ProQuest Central Essentials AUTh Library subscriptions: ProQuest Central Technology Collection ProQuest One Community College Middle East & Africa Database ProQuest Central Engineering Research Database Aerospace Database SciTech Premium Collection ProQuest Engineering Collection Advanced Technologies Database with Aerospace Engineering Database Advanced Technologies & Aerospace Database ProQuest Advanced Technologies & Aerospace Collection Publicly Available Content (ProQuest) ProQuest One Academic Eastern Edition (DO NOT USE) ProQuest One Academic ProQuest One Academic UKI Edition ProQuest Central China Engineering Collection Open Access: DOAJ - Directory of Open Access Journals |
DatabaseTitle | CrossRef Publicly Available Content Database Technology Collection Technology Research Database Mechanical & Transportation Engineering Abstracts ProQuest Advanced Technologies & Aerospace Collection ProQuest Central Essentials ProQuest Central (Alumni Edition) SciTech Premium Collection ProQuest One Community College ProQuest Central China ProQuest Central Aerospace Database ProQuest Engineering Collection Middle East & Africa Database ProQuest Central Korea Advanced Technologies Database with Aerospace Engineering Collection Advanced Technologies & Aerospace Collection Engineering Database ProQuest One Academic Eastern Edition ProQuest Technology Collection ProQuest SciTech Collection Advanced Technologies & Aerospace Database ProQuest One Academic UKI Edition Materials Science & Engineering Collection Engineering Research Database ProQuest One Academic |
DatabaseTitleList | CrossRef Publicly Available Content Database |
Database_xml | – sequence: 1 dbid: RHX name: Open Access Journals (Hindawi Publishing) url: http://www.hindawi.com/journals/ sourceTypes: Publisher – sequence: 2 dbid: DOA name: DOAJ Directory of Open Access Journals url: https://www.doaj.org/ sourceTypes: Open Website – sequence: 3 dbid: 8FG name: ProQuest Technology Collection url: https://search.proquest.com/technologycollection1 sourceTypes: Aggregation Database |
DeliveryMethod | fulltext_linktorsrc |
Discipline | Engineering |
EISSN | 1687-5974 |
Editor | Kayacan, Erkan |
Editor_xml | – sequence: 1 givenname: Erkan surname: Kayacan fullname: Kayacan, Erkan – fullname: Erkan Kayacan |
EndPage | 12 |
ExternalDocumentID | oai_doaj_org_article_4ec84e5dc8ee489bace7099f4d0ac234 10_1155_2022_6439787 |
GrantInformation_xml | – fundername: National Natural Science Foundation of China grantid: 52006099 – fundername: Six Talent Peaks Project in Jiangsu Province grantid: 2016-HKHT-017 – fundername: Fundamental Research Funds for the Central Universities grantid: 309181B8812; 30920021102 |
GroupedDBID | 188 29J 2WC 3V. 4.4 5GY 5VS 8FE 8FG 8R4 8R5 AAFWJ AAJEY ABDBF ABJCF ABUWG ACIWK ADBBV AEGXH AENEX AFKRA AFPKN AINHJ ALMA_UNASSIGNED_HOLDINGS ARAPS BCNDV BENPR BGLVJ BPHCQ CCPQU CS3 CWDGH E3Z EBS ESX GROUPED_DOAJ HCIFZ I-F IAO IEA ISR ITC KQ8 L6V M7S MK~ M~E OK1 P62 PIMPY PQQKQ PROAC PTHSS Q2X RHU RHW RHX RNS TR2 TUS UNMZH ~8M 24P AAYXX CITATION H13 7TB 8FD AZQEC DWQXO FR3 H8D L7M PQEST PQUKI PRINS |
ID | FETCH-LOGICAL-c403t-779c263ea004f55951c7b085430c05b3c8f5eb5143559bda3a9f293c5cb697ce3 |
IEDL.DBID | DOA |
ISSN | 1687-5966 |
IngestDate | Fri Oct 04 13:15:11 EDT 2024 Fri Sep 13 09:46:49 EDT 2024 Fri Aug 23 02:50:05 EDT 2024 Sun Jun 02 19:22:09 EDT 2024 |
IsDoiOpenAccess | true |
IsOpenAccess | true |
IsPeerReviewed | true |
IsScholarly | true |
Language | English |
License | This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. |
LinkModel | DirectLink |
MergedId | FETCHMERGED-LOGICAL-c403t-779c263ea004f55951c7b085430c05b3c8f5eb5143559bda3a9f293c5cb697ce3 |
ORCID | 0000-0002-8854-5720 0000-0002-1483-9101 |
OpenAccessLink | https://doaj.org/article/4ec84e5dc8ee489bace7099f4d0ac234 |
PQID | 2740359105 |
PQPubID | 237291 |
PageCount | 12 |
ParticipantIDs | doaj_primary_oai_doaj_org_article_4ec84e5dc8ee489bace7099f4d0ac234 proquest_journals_2740359105 crossref_primary_10_1155_2022_6439787 hindawi_primary_10_1155_2022_6439787 |
PublicationCentury | 2000 |
PublicationDate | 2022-00-00 |
PublicationDateYYYYMMDD | 2022-01-01 |
PublicationDate_xml | – year: 2022 text: 2022-00-00 |
PublicationDecade | 2020 |
PublicationPlace | New York |
PublicationPlace_xml | – name: New York |
PublicationTitle | International journal of aerospace engineering |
PublicationYear | 2022 |
Publisher | Hindawi Hindawi Limited Wiley |
Publisher_xml | – name: Hindawi – name: Hindawi Limited – name: Wiley |
References | 23 45 46 47 26 M. B. Padwal (37) 2018; 190 28 29 L. Ping (40) 2009; 15 A. N. Ali (42) 2005; 30 H. M. Wang (24) 2015; 36 31 S. P. Zhou (6) 2020; 43 10 11 12 L. Kong (22) 2020; 43 13 14 C. Y. Tu (30) 36 15 16 F. Q. Zhao (33) 2002; 23 38 17 39 18 19 W. Zhang (44) 1999; 7 Y. J. Luo (2) 2007; 15 H. S. Xiang (25) 2016; 39 J. C. Zhao (35) 2019; 42 C. Y. Tu (27) 2022; 30 1 3 4 5 7 8 9 L. Zheng (32) 2010; 18 Z. R. Liu (34) 2007; 30 41 20 21 43 |
References_xml | – volume: 18 start-page: 180 issue: 2 year: 2010 ident: 32 article-title: Effect of magnesium powder particle size on combustion properties of Mg/PTFE fuel-rich propellant publication-title: Chinese Journal of Energetic Materials contributor: fullname: L. Zheng – ident: 8 doi: 10.2514/3.3011 – ident: 14 doi: 10.1016/S0010-2180(01)00281-4 – ident: 16 doi: 10.1016/j.combustflame.2011.06.020 – ident: 46 doi: 10.1615/IntJEnergeticMaterialsChemProp.2013005557 – ident: 23 doi: 10.4028/www.scientific.net/AMR.549.1037 – volume: 7 start-page: 118 issue: 3 year: 1999 ident: 44 article-title: Research on test method of combustion performance of lean oxygen propellant at low pressure publication-title: Chinese Journal of Energetic Materials contributor: fullname: W. Zhang – volume: 15 start-page: 28 issue: 2 year: 2009 ident: 40 article-title: Study on laser ignition characteristics of a high energy propellant publication-title: Journal of Gun Launch and Control contributor: fullname: L. Ping – ident: 7 doi: 10.1007/s10973-020-09297-4 – ident: 17 doi: 10.1002/prep.201500080 – ident: 43 doi: 10.1016/j.combustflame.2013.02.019 – ident: 26 doi: 10.1002/prep.201700059 – volume: 15 start-page: 407 issue: 4 year: 2007 ident: 2 article-title: Research progress of high energy solid propellant publication-title: Chinese Journal of Energetic Materials contributor: fullname: Y. J. Luo – ident: 30 article-title: Dynamic behavior study of aluminum aggregates on the NEPE propellant combustion surface [J/OL] publication-title: Journal of Propulsion Technology contributor: fullname: C. Y. Tu – volume: 36 start-page: 1262 issue: 8 year: 2015 ident: 24 article-title: Study on ignition and combustion characteristics of NEPE propellant under laser irradiation publication-title: Journal of Propulsion Technology contributor: fullname: H. M. Wang – ident: 21 doi: 10.1002/cjoc.201090132 – volume: 30 start-page: 57 issue: 5 year: 2007 ident: 34 article-title: Investigation on thermal decomposition of mixed systems of AP with RDX and HMX by DSC-TG-FTIR publication-title: Chinese Journal of Explosives & Propellants contributor: fullname: Z. R. Liu – ident: 18 doi: 10.1002/prep.201700191 – ident: 15 doi: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.300 – volume: 30 start-page: 811 issue: 8 year: 2022 ident: 27 article-title: Ignition and combustion characteristics of NEPE propellant in nitrogen and air publication-title: Chinese Journal of Energetic Materials contributor: fullname: C. Y. Tu – volume: 42 start-page: 380 issue: 4 year: 2019 ident: 35 article-title: Effect AP on the thermal stability of RDX and detonation performance of AP/RDX publication-title: Chinese Journal of Explosive & Propellants contributor: fullname: J. C. Zhao – ident: 1 doi: 10.1002/prep.201600131 – ident: 13 doi: 10.2514/3.51071 – ident: 36 doi: 10.1016/j.tca.2015.04.025 – ident: 39 doi: 10.1080/00102200302358 – ident: 9 doi: 10.2514/3.3213 – volume: 30 start-page: 351 issue: 5 year: 2005 ident: 42 article-title: Laser ignition of DAAF, DHT and DAATO (3.5) publication-title: Propellants Explosives Pyrotechnics doi: 10.1002/prep.200500025 contributor: fullname: A. N. Ali – volume: 23 start-page: 249 issue: 3 year: 2002 ident: 33 article-title: Study on the thermal decomposition of NEPE propellant (I) thermal decomposition of binder publication-title: Journal of Propulsion Technology contributor: fullname: F. Q. Zhao – ident: 11 doi: 10.1080/00102207308946646 – ident: 29 doi: 10.1016/j.dt.2022.05.016 – ident: 38 doi: 10.1016/j.jhazmat.2017.08.055 – volume: 43 start-page: 195 issue: 2 year: 2020 ident: 6 article-title: Influence of CL-20 content and particle size gradation on combustion performance of NEPE propellant publication-title: Chinese Journal of explosives & propellants contributor: fullname: S. P. Zhou – ident: 47 doi: 10.1002/prep.202000170 – ident: 41 doi: 10.1016/S0082-0784(71)80105-4 – volume: 43 start-page: 432 issue: 4 year: 2020 ident: 22 article-title: Study on mechanisms of AP decomposition and NEPE propellant oxygenizing and cross-linking publication-title: Journal of Solid Rocket Technology contributor: fullname: L. Kong – ident: 45 doi: 10.1023/A:1017561827203 – ident: 3 doi: 10.1155/2020/8858057 – volume: 190 start-page: 1 issue: 9 year: 2018 ident: 37 article-title: Thermal decomposition and combustion characteristics of HTPB-coarse AP composite solid propellants catalyzed with Fe2O3 publication-title: Combustion Science and Technology doi: 10.1080/00102202.2018.1460599 contributor: fullname: M. B. Padwal – ident: 5 doi: 10.1002/prep.202000326 – ident: 10 doi: 10.1080/00102207508946677 – ident: 12 doi: 10.1016/0010-2180(79)90008-7 – ident: 19 doi: 10.1002/prep.201600291 – ident: 20 doi: 10.3390/molecules25102276 – ident: 28 doi: 10.13224/j.cnki.jasp.20220229 – ident: 4 doi: 10.1016/j.dt.2020.09.020 – ident: 31 doi: 10.2514/1.36458 – volume: 39 start-page: 75 issue: 3 year: 2016 ident: 25 article-title: Effect of oxygen content in environment gas on the laser ignition process of NEPE propellant publication-title: Chinese Journal of Explosives and Propellants contributor: fullname: H. S. Xiang |
SSID | ssj0060575 ssib005317291 |
Score | 2.2552485 |
Snippet | Nitrate ester plasticized polyether (NEPE) propellant is widely used in solid rocket motors, having both good mechanical properties and high specific impulse.... |
SourceID | doaj proquest crossref hindawi |
SourceType | Open Website Aggregation Database Publisher |
StartPage | 1 |
SubjectTerms | Aerospace engineering Aluminum Burning rate Chemical reactions Combustion chambers Decomposition Delay time Energy Experiments Flammability Flammable gases Gasification Heat Heat flux High speed cameras Ignition Influence Lasers Mechanical properties Oxidation Polyethylene glycol Polyvinyl chloride Pressure Solid propellant rocket engines Specific impulse Thermal decomposition Thermogravimetry |
SummonAdditionalLinks | – databaseName: Open Access Journals (Hindawi Publishing) dbid: RHX link: http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwjV27TsMwFLWgEwyIpygU5KFsBNLaTpyRR6uCBKoQlbpFfgoklKAShGBiYGHmD_slXLsuKjDAGCtyFF9f33OS42OEmlyrJJUyi2CF1BHVRkacExEJpVtUtLzHt1NbXCa9AT0fsmEwSXr4_Qsfqp2j5-1DXzh5Oo_mOXcW-Ve94ew0Aoj4pexIHARxPCuB_GEA56d69x99fatE3rAfMPCNY8JPt79WZl9uustoKeBEfDQJ7AqaM8UqWpxxD1xDbxBiWFbv8KlxwvCgvtrHZ14QVBY4bALAotAY8l66g7ugOVgijnBp8eWtd6fFHeeXgPsApZ3K-sVo3C_vnv1mYNeN10gVFRYVhlccv36Qg3j8-n7RF-to0O1cn_SicKhCpGhMKkDTmWonxAjIDgt0grVUKgF3URKrmEmiuGVGehjFMqkFEZkFSKCYkkmWKkM2UK0oC7OJMJfCxlJZklhNpVSCZCITwK-Ag9lExnW0Nx3g_H7inZF7zsFY7gKRh0DU0bEb_a97nOO1b4BZkIcEyqlRnBqmFTeG8kwKZVJAt5bqWKg2oXXUDLH741mNaWDzkK0POTBz52QIUHPrf71sowV3OfkU00C1avRodgCcVHLXT81Pfl7cyg priority: 102 providerName: Hindawi Publishing – databaseName: AUTh Library subscriptions: ProQuest Central dbid: BENPR link: http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwhV1Nb9QwELVKe4ED4lMslMqHciNsdm1nkxOidKsFidUKUam3yDO2aaUqKUuqCk49cOm5_7C_hBmvU1ZCgqsTOYrnw2_s52chdkuHxQSgyihDukw7D1lZKptZdCNtR1Hjm9kW82J2qD8emaMNMevPwjCtss-JMVG7FnmNfEjVE6vNERwYWuBVAOyGb8--ZXx_FO-zpss07oit8Ujzhu3W3nS--Lzua4Qjb-kfBeMULsYKCjJDmL8nxRvD6wHjYZypmWi3Nl1FVX8CysdcLl-c_JW-45x08EDcT2BSvltZ_6HY8M0jcW9NYvCx-EV-QLn3VO57Zo8nitZr-SGyhtpGppMC0jZOUnIAvt2LmpNu4lK2Qc5PooStnLKoglwQ3mYq9k_v5KI9_RFPDHM3kUjVdNJ2kn7x5vJavclvLq8-LewTcXgw_fJ-lqWbFzKkUe4Iclc4LpS3FEKBag4zwgkQONMqx9yAwjIYDxFrmQqcVbYKhBvQIBTVBL16KjabtvHPhCzBhhwwqCI4DYBWVbayVIRRoRYKyAfiVT_A9dlKYKOOhYkxNRuiToYYiD0e_dt3WBY7NrTLr3WKslp7LLU3DkvvdVmBRT8hCBy0yy2OlR6I3WS7_3xruzdsnUL6e_3HAZ__-_ELcZc7W63TbIvNbnnuXxJy6WAnOeVv-6Xr_w priority: 102 providerName: ProQuest |
Title | Thermal Decomposition, Ignition Process and Combustion Behavior of Nitrate Ester Plasticized Polyether Propellant at 0.1–3.0 MPa |
URI | https://dx.doi.org/10.1155/2022/6439787 https://www.proquest.com/docview/2740359105/abstract/ https://doaj.org/article/4ec84e5dc8ee489bace7099f4d0ac234 |
Volume | 2022 |
hasFullText | 1 |
inHoldings | 1 |
isFullTextHit | |
isPrint | |
link | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwrV07T8MwGLSgLDAgnqJQKg9lI5DWduqMPFoKElVVgdQt8lNUqlIEQQgmBhZm_iG_hM-OiyoxsLBksKI48cWf76LLGaEG1yppS5lGUCF1RLWREedERELpJhVNn_Ht3Bb9pHdLr0ZsNLfVl_OElfHA5cAdU6M4NUwrbgzlqRTKtIHVWKpjoVqkTAJtspmYKmtw4ljIzObOmFP4rWO_9jrr3NwC5HP6gfreOQH8PP5VkP0q011Dq4Ee4pPyttbRgsk30MpcaOAmegdkoZpO8LlxfvBgujrEl94HNM1x8P5jkWsM0126_bqgOSQhPuCpxf2xD6XFHReTgAfAoJ25-tVoPJhOXvw_wO4y3hqVF1gUGB7x6-2THMVfbx_XA7GFbrudm7NeFPZSiBSNSQEkOlWthBgBk8KCimBN1ZZAtyiJVcwkUdwyIz17YqnUgojUAhNQTMkkbStDtlEln-ZmB2EuhY2lsiSxmkqpBElFKkBWgfSyiYyr6GA2wNl9GZmReanBWOaAyAIQVXTqRv_nHBd07RsA_izAn_0FfxU1AnZ_9FWbAZuFSfqYgSB3AYbAMHf_41b20LLrsvw-U0OV4uHJ7ANjKWQdLfLuRR0tnXb6g2Hdv6pwHPZG37LJ7tc |
link.rule.ids | 315,786,790,869,870,883,884,2115,4043,12792,21416,27956,27957,27958,33408,33779,43635,43840,74392,74659 |
linkProvider | Directory of Open Access Journals |
linkToHtml | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwhV1LT9wwELZ4HEoPVelDXUrBB3prSnZtZ5NT1QfbpYXVHkDiZtljm66EEroEVeXEgUvP_Yf8ks54vbBSpfaaRI7i8cx843z-hrGd0kHRt7bKMEK6TDpvs7IUJjPgutJ0o8Y3sS1GxfBYfjlRJ2nD7SLRKucxMQZq1wDtke9i9URqcwgH3p1_z6hrFP1dTS00ltmqFJg66aT44PPi-kLseEf5KAibUAFWoGMpxPlzIrxStAfQ243Zmch1CykqKvkjOP5GJfKPyV8hO-ahwWP2KAFI_n5m8XW25Osn7OGCrOBTdoO2x3h7xj95YownWtYbvh-ZQk3N0-kAbmrHMSBY6uiFl5NW4pQ3gY8mUbaW75GQAh8jxib69ZV3fNyc_YynhGmYSJ6qW25ajp94e_1bvM1vr38djs0zdjzYO_o4zFK3hQxwZluE2RX0CuENuk3AOkN1oW8RkEmRQ66sgDIobyO-UpV1RpgqIFYABbao-uDFc7ZSN7V_wXhpTcgtBFEEJ60FIypTGSy8sDgLhc077PV8gvX5TFRDx2JEKU2G0MkQHfaBZv_uGZLCjhea6alOnqWlh1J65aD0XpaVNeD7CHuDdLmBnpAdtpNs9593bc4Nq5MbX-j7Rbfx79vb7MHw6PBAH-yPvr5kazTwbJ9mk62000v_CpFLa7fi8vwDx6npzA |
linkToPdf | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwhV1NT9RAGJ4oJEYPRFDDKh9zwJt1uzsfbU9GZDeguGmMJNwm8wkkpMWlxuCJgxfP_kN-Ce87OwubmOi1babpvB_zvNNnnpeQndJZWRhTZZAhXcadN1lZMp1p6wZcD6LGN7ItJnL_iH88FseJ_3SZaJXznBgTtWst7pH3oXpCtTmAA_2QaBH13vjdxbcMO0jhn9bUTuMhWS64FODhy7ujSf1l0dsASd4RQCQiFSzHJISZANQ_p8ULgTsCw35cq5Fqt7BgRV1_gMqnWDD_OPsrgcdVafyUrCQ4Sd_P7L9KHvhmjTxZEBl8Rn6BJ0D2Pad7HvnjiaT1hh5E3lDb0HRWgOrGUUgPBvt7weWknDilbaCTsyhiS0coq0BrQNxIxv7pHa3b86t4ZhiHiVSqpqO6o_CJN9d_2Nv85vr351o_J0fj0dcP-1nqvZBZmOcOQHdlh5J5DUEUoOoQA1sYgGec5TYXhtkyCG8i2hKVcZrpKgBysMIaWRXWsxdkqWkbv05oaXTIjQ1MBseNsZpVutJQhkGpFqTJe-T1fILVxUxiQ8XSRAiFhlDJED2yi7N_9wwKY8cL7fREpThT3NuSe-Fs6T0vK6OtLwAEB-5ybYeM98hOst1_3rUxN6xKQX2p7l3w5b9vb5NH4Jvq8GDy6RV5jOPONm02yFI3_e43AcZ0Ziv55y3nJO9v |
openUrl | ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Ajournal&rft.genre=article&rft.atitle=Thermal+Decomposition%2C+Ignition+Process+and+Combustion+Behavior+of+Nitrate+Ester+Plasticized+Polyether+Propellant+at+0.1%E2%80%933.0%E2%80%89MPa&rft.jtitle=International+journal+of+aerospace+engineering&rft.au=Chengyin+Tu&rft.au=Yaya+Feng&rft.au=Zhigang+Ling&rft.au=Xiong+Chen&rft.date=2022&rft.pub=Wiley&rft.eissn=1687-5974&rft.volume=2022&rft_id=info:doi/10.1155%2F2022%2F6439787&rft.externalDBID=DOA&rft.externalDocID=oai_doaj_org_article_4ec84e5dc8ee489bace7099f4d0ac234 |
thumbnail_l | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=1687-5966&client=summon |
thumbnail_m | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=1687-5966&client=summon |
thumbnail_s | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=1687-5966&client=summon |