Experimental study of rheology and combustion characteristics of solidified ethanol fuel for hybrid rocket engine = 하이브리드 로켓용 고형화된 에탄올의 유변학적 및 연소특성에 관한 실험적 연구
서명 / 저자 Experimental study of rheology and combustion characteristics of solidified ethanol fuel for hybrid rocket engine = 하이브리드 로켓용 고형화된 에탄올의 유변학적 및 연소특성에 관한 실험적 연구 / Jerin John.
저자명 John, jerin ; 전제린
발행사항 [대전 : 한국과학기술원, 2018].
Online Access 원문보기 원문인쇄





학술문화관(문화관) 보존서고

DAE 18033







The study reports first findings on the solidi cation of eco-friendly ethanol fuel by organic gellant, namely Methylcellulose (MC) and Hydroxypropyl methylcellulose (HPMC) for use as a solid fuel for the hybrid propulsion system. Molecular interaction studies using fourier transform infrared spectroscopy (FTIR) reveals that the intra- and inter-molecular hydrogen bonding increases with increase in MC/HPMC. However, from the thermal studies using dynamic scattering calorimetry (TMDSC) and Thermogravimetric analysis (TGA, the melting temperature (Tm) and onset of decomposition temperature ($T_{(d,onset)}$) lies close for all the samples (~ $60^\circ C $). The apparent activation energy (Ea) of the solidified ethanol is determined using is-conversional Friedman method from TGA. Ea is found to be in the range of 9.06-14.01 kJ/mol and found to decrease with increase in the gellant concentration. The rheological properties of solidified ethanol (SE) are determined using both shear flow tests and dynamic oscillation tests for the gellant concentration varying in the range of 5 wt.% to 17 wt.% and nanoparticle loading varying in the range of 2 wt.% to 6 wt.% for HPMC and 2 wt.% to 4 wt.% for MC samples respectively. It is observed that over the range of applied shear rate (0.1- 1000 $s^{-1}$) solidified ethanol fuels exhibit a strong shear thinning, high yield thixotropic behavior. The yield stress of the fuel sample ranges from 424.20- 1252.40 Pa, and found to the direct function of type, concentration of gellant and nanoparticle loading. Below the yield stress, the solid samples exhibit an elastic dominant behavior (G'>G") and found to be independent of applied stress in the linear viscoelastic region. In dynamic tests, the spectra of G'($\omega$) and G"($\omega$) indicates that solidified ethanol forms a covalently cross-linked network between ethanol-water blend and gellant material. A key finding of this study reveals that all ethanol fuel formulations display solid-like characteristics under test conditions as G' and G" are nearly independent of the frequency and the magnitude of G' is 4.1-5.4 times higher than G". The effect of gellant type on rheological behavior is studied where it is observed that the relative thixotropic area and creep strain of HPMC laden fuels is significantly higher compared to their MC counterparts which imparts them a viscous dominant character. The hypergolic ignition delays of the SE fuels with rocket grade hydrogen peroxide (90 %RGHP; $H_2O_2$) are investigated using manganese (III) acetylacetonate (Mnacac) as a catalyst and found that the ID value lies in the range of 41 -307 ms from the drop-test. A key finding from the hypergolic study is that a minimum catalyst concentration ($[C]_{Mn3+;L}$) is required to ignite SE fuel using $H_2O_2$ and ID decreases with increase in the $[C]_{Mn3+}$. Similarly, there exist an upper catalyst loading ($[C]_{Mn3+;L}$) above which ID is increased or not improved. For MC case $[C]_{Mn3+;U}$=18 wt.% and HPMC case $[C]_{Mn3+;U}$=16 wt.%. Additionally, ID is found to be directly depended on the type and concentration of the gellant ([C]g). Finally, SEM-EDS analysis of the residue indicates the formation of oxides of Manganese with a small amount of Carbon (~1.66 to 2.53 wt.%) hinting a complete combustion of the gellant particles. The reaction-driven SE fuel is formulated using metal salt $FeCl_3$ with HPMC and predicted the possible solidi cation mechanism using FTIR. It is found that the solidi cation of ethanol using $FeCl_3$ is the interplay between hydrogen bonding and ionic bond formed between HPMC and $Fe^{3+}$ ion. The ignition delay for reaction-driven fuels are in the range of 588.0-787.6 ms and observed to be higher in comparison with catalytically promoted SE fuels. Furthermore, when the temperature of the fuel was raised from room temperature to $80^\circ C $, the ID was lowered by ~71 % indicating a strong dependence of temperature on reaction rate. Finally the regression rate ($\dot{r}_b$) of the unloaded SE fuels is determined using in-house designed opposed flow burner with gaseous oxygen (GOX) at varying oxidizer mass flux ranges from 0.97 to 11.7 kg/$m^2$-s. The $\dot{r}_b$ is found to increase with increasing oxidizer mass flux, a typical hybrid solid fuel behavior. $\dot{r}_b$ value lies in the close range with the maximum value observed to be 0.22 mm/s at 11.7 kg/$m^2$-s for the HPMC 10 fuel. Furthermore, an increase of 67% in the $\dot{r}_b$ is observed when HPMC 10 fuel was loaded with 4 wt.% of nano-Al particles at 11.7 kg/$m^2$-s. From the hypergolic and regression rate experiments, it is observed that the solidi cation technique using organic gellants for liquid fuels have a potential to create eco-friendly, high-regressive hypergolic fuel for the next generation hybrid rocket engines.

이 연구는 하이브리드 추진 시스템의 고체 연료로 사용되는 유기 젤화제, 즉 Methylcellulose (MC) 및 Hydroxypropyl methylcellulose (HPMC)에 의한 친환경 에탄올 연료의 고형화에 대한 연구이다. 퓨리에 변환 적외선 분광법(FTIR)을 이용한 분자 상호 작용 연구결과 젤화제(MC/HPMC)가 증가함에 따라 분자간 수소 결합이 증가한다는 것으로 나타났다. 고형화 에탄올(Solidified Ethanol SE)의 겉보기 활성화 에너지 ($E_a$)는 TGA에서 기존의 Friedman 방법을 사용하여 결정하였으며, ($E_a$)는 9.06 - 14.01 kJ/mol의 범위에 있고 사용된 젤화제의 양이 증가함에 따라 감소하는 것으로 나타났다. 고형화 에탄올을 만들기 위해 사용된 젤화제의 양은 5 wt. % ~ 17 wt. % 이며, HPMC 젤화제의 경우 첨가한 알루미늄 나노 입자의 양은 2 wt. % ~ 6 wt. %, MC 젤화제의 경우 첨가된 알루미늄 나노 입자의 양은 2 wt. % ~ 4 wt. % 이다. 고형화 에탄올(SE) 의 유변학적 특성은 시료의 전단 유동 시험 및 동적 진동 시험을 사용하여 측정 하였다. 고형화 에탄올 연료는 shear rate(0.1- 1000 $s^{-1}$)의 범위에 걸쳐 강한 전단 박화 현상과, 요변성 현상을 보였다. 연료 시료의 항복 응력 범위는 424.20-1252.40 Pa이며, 젤화제의 농도와 나노 입자의 첨가량에 비례하였다. 로켓 등급의 과산화수소(90 % RGHP; $H_2O_2$)를 사용한 SE연료의 점화지연시간은, manganese(III) acetylacetonate(Mnacac) 촉매의 낙하 테스트에서 41-307 ms 로 측정되었다. 0.97 - 11.7 kg/$m^2$-s 의 범위의 산소 공급량에 따라 변화하는 SE 연료의 regression rate ($\dot{r}_b$b)를 측정하였다. $\dot{r}_b$b 값은 공급되는 산화제의 양이 증가함에 따라 증가하는 것으로 나타났다. HPMC 10 연료의 경우 11.7 kg/m2-s 의 산소 공급 환경에서 $\dot{r}_b$b는 0.22 mm/s의 최대값을 보였고, 이 조건에 알루미늄 나노 입자가 4 wt. % 첨가 되었을 때 $\dot{r}_b$b 가 67% 증가하는 것으로 관측 되었다.


청구기호 {DAE 18033
형태사항 vii, 82 p. : 삽도 ; 30 cm
언어 영어
일반주기 저자명의 한글표기 : 전제린
지도교수의 영문표기 : Seung Wook Baek
지도교수의 한글표기 : 백승욱
수록잡지명 : "Rheology of solid-like ethanol fuel for hybrid rockets: Effect of type and concentration of gellants". Fuel, v.209, pp.96-108(2017)
학위논문 학위논문(박사) - 한국과학기술원 : 항공우주공학과,
서지주기 References : p. 71-76
주제 Solidified ethanol
hybrid rocket fuel
hypergolic ignition
regression rate
고형화 에탄올
하이브리드 로켓 연료
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