Minkyo Seo , Vikas K. Bhosale , Hyeonjun Im , Sejin Kwon
{"title":"Performance improvement of triglyme-based fuels using an ionic liquid with hydrogen peroxide","authors":"Minkyo Seo , Vikas K. Bhosale , Hyeonjun Im , Sejin Kwon","doi":"10.1016/j.combustflame.2024.113719","DOIUrl":null,"url":null,"abstract":"<div><p>Low-toxicity hypergolic propellants have been a demanding research area in recent years for space propulsion, with the aim of replacing conventional toxic propellants. Therefore, the current research was focused on the development of low-toxicity hypergolic propellants for safe, cost-effective, and sustainable space exploration. In this study, triglyme was selected as a fuel component for the low-toxicity hypergolic propellant. Hypergolic performance of various concentrations (3 to 13 wt%) of monocyanotrihydroborate tetrakis(imidazole) copper(II) cyanotrihydroborate additive (Cu-P1) in triglyme fuel was experimentally investigated with 70, 90 and 95 wt% hydrogen peroxide (H<sub>2</sub>O<sub>2</sub>). The new fuels, 13Cu-TriG and 13Cu-TriGIL, containing 13 wt% of Cu-P1 in triglyme and triglyme:1-ethyl-3-methyl imidazolium cyanoborohydride ([EMIM][BH<sub>3</sub>CN]) blend, respectively, were investigated. The hypergolic performance and properties of triglyme were improved by using [EMIM][BH<sub>3</sub>CN]. For example, 13Cu-TriG was not ignited with 70 wt% H<sub>2</sub>O<sub>2</sub>; however, 13Cu-TriGIL exhibited an IDT of 16.5 ms. Furthermore, 13Cu-TriG and 13Cu-TriGIL revealed an IDT of 18.7 and 8.0 ms, respectively, with 95 wt% H<sub>2</sub>O<sub>2</sub>. The physicochemical properties, such as density, viscosity, decomposition temperature, and freezing/melting temperature, of 13Cu-TriG and 13Cu-TriGIL, were also measured. 13Cu-TriGIL showed a density of 1.017 g/cm<sup>3</sup> and a viscosity of 26.42 mPa·s. Additionally, 13Cu-TriG exhibited a freezing point of −45 °C. However, with the addition of [EMIM][BH<sub>3</sub>CN] in the fuel, the freezing temperature drops below −80 °C (13Cu-TriGIL). Furthermore, 13Cu-TriGIL with 95 wt% H<sub>2</sub>O<sub>2</sub> demonstrated theoretical specific impulse and density specific impulse of 2.1 % lower and 9.7 % higher than MMH/NTO, respectively. Overall, the use of ionic liquid to improve the hypergolic performance and physicochemical properties of triglyme-based fuels was the advantage of our research.</p></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"270 ","pages":"Article 113719"},"PeriodicalIF":5.8000,"publicationDate":"2024-09-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Combustion and Flame","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0010218024004280","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENERGY & FUELS","Score":null,"Total":0}
引用次数: 0
Abstract
Low-toxicity hypergolic propellants have been a demanding research area in recent years for space propulsion, with the aim of replacing conventional toxic propellants. Therefore, the current research was focused on the development of low-toxicity hypergolic propellants for safe, cost-effective, and sustainable space exploration. In this study, triglyme was selected as a fuel component for the low-toxicity hypergolic propellant. Hypergolic performance of various concentrations (3 to 13 wt%) of monocyanotrihydroborate tetrakis(imidazole) copper(II) cyanotrihydroborate additive (Cu-P1) in triglyme fuel was experimentally investigated with 70, 90 and 95 wt% hydrogen peroxide (H2O2). The new fuels, 13Cu-TriG and 13Cu-TriGIL, containing 13 wt% of Cu-P1 in triglyme and triglyme:1-ethyl-3-methyl imidazolium cyanoborohydride ([EMIM][BH3CN]) blend, respectively, were investigated. The hypergolic performance and properties of triglyme were improved by using [EMIM][BH3CN]. For example, 13Cu-TriG was not ignited with 70 wt% H2O2; however, 13Cu-TriGIL exhibited an IDT of 16.5 ms. Furthermore, 13Cu-TriG and 13Cu-TriGIL revealed an IDT of 18.7 and 8.0 ms, respectively, with 95 wt% H2O2. The physicochemical properties, such as density, viscosity, decomposition temperature, and freezing/melting temperature, of 13Cu-TriG and 13Cu-TriGIL, were also measured. 13Cu-TriGIL showed a density of 1.017 g/cm3 and a viscosity of 26.42 mPa·s. Additionally, 13Cu-TriG exhibited a freezing point of −45 °C. However, with the addition of [EMIM][BH3CN] in the fuel, the freezing temperature drops below −80 °C (13Cu-TriGIL). Furthermore, 13Cu-TriGIL with 95 wt% H2O2 demonstrated theoretical specific impulse and density specific impulse of 2.1 % lower and 9.7 % higher than MMH/NTO, respectively. Overall, the use of ionic liquid to improve the hypergolic performance and physicochemical properties of triglyme-based fuels was the advantage of our research.
期刊介绍:
The mission of the journal is to publish high quality work from experimental, theoretical, and computational investigations on the fundamentals of combustion phenomena and closely allied matters. While submissions in all pertinent areas are welcomed, past and recent focus of the journal has been on:
Development and validation of reaction kinetics, reduction of reaction mechanisms and modeling of combustion systems, including:
Conventional, alternative and surrogate fuels;
Pollutants;
Particulate and aerosol formation and abatement;
Heterogeneous processes.
Experimental, theoretical, and computational studies of laminar and turbulent combustion phenomena, including:
Premixed and non-premixed flames;
Ignition and extinction phenomena;
Flame propagation;
Flame structure;
Instabilities and swirl;
Flame spread;
Multi-phase reactants.
Advances in diagnostic and computational methods in combustion, including:
Measurement and simulation of scalar and vector properties;
Novel techniques;
State-of-the art applications.
Fundamental investigations of combustion technologies and systems, including:
Internal combustion engines;
Gas turbines;
Small- and large-scale stationary combustion and power generation;
Catalytic combustion;
Combustion synthesis;
Combustion under extreme conditions;
New concepts.