• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2011.11a
• /
• pp.869-872
• /
• 2011

Ignition tests of an oxidizer rich preburner for a staged combustion cycle liquid rocket engine were performed to evaluate combustion performance. Design operation conditions of the tested oxidizer rich preburner are about 60 of OF ratio and 20 MPa of combustion pressure. The entire kerosene and some LOx injected into the mixing head is burned in combustion chamber and the remaining LOx injected through center holes of combustion chamber is vaporized. Full flow ignition method with hypergolic fuel was used. Each propellant was supplied in two stages for soft ignition. Test results, low frequency oscillation was occurred in low flow rate conditions under 45% of design flow rate. Stable ignition in the course of design combustion pressure was able to induce by minimization of low flow rate ignition region to escape low frequency oscillation.

• Proceedings of the Korean Environmental Sciences Society Conference
• /
• 2008.11a
• /
• pp.464-467
• /
• 2008

성능이 우수한 다성분계 전극을 개발하기 위하여 Pt, Ru, Sn, Sb 및 Gd의 5 종류 금속을 이용하여 1성분계 전극의 성능과 산화제 생성량 및 2성분계 전극의 성능과 산화제 생성 경향을 고찰하여 다음의 결과를 얻었다. 1. RhB 농도 감소는 Ru/Ti > Sb/Ti > Pt/Ti > Sn/Ti > Gd/Ti 전극의 순서로 나타났으나 단위 전력당 2분간 제거된 RhB 농도 감소는 Ru/Ti > Sb/Ti > Pt/Ti > Gd/Ti > Sn/Ti 전극의 순서로 나타났다. 생성된 산화제 농도는 ClO$_2$ > free Cl > H$_2$O$_2$ > O$_3$의 순서였으며 Gd/Ti 전극의 경우 산화제가 거의 생성되지 않는 것으로 나타났다. 모든 전극에서 OH 라디칼이 거의 생성되지 않는 것으로 나타났다. Ru/Ti와 Sb/Ti 전극의 높은 RhB 분해와 산화제 생성 농도는 정확하지는 않지만 상관관계가 있는 것으로 나타났다. 2. Ru계 2성분 전극(Ru-Gd/Ti, Ru-Pt/Ti, Ru-Sn/Ti 및 Ru-Sb/Ti)은 모두 1성분계 전극보다 RhB 분해성능이 높아지는 것으로 나타났으며, Ru계 2성분 전극 중 가장 성능이 우수하였던 전극은 Ru:Sn=9:1 전극으로 나타났다. Sn-Sb/Ti 전극은 Sn:Sb=1:9의 전극 성능이 우수한 것으로 나타났으나 Sb/Ti 전극과의 차이는 크지 않은 것으로 나타났다. Pt계 전극(Pt-Gd/Ti, Pt-Sn/Ti, Pt-Sb/Ti)은 대체로 두 성분 혼합에 따른 RhB 분해효과 상승은 없는 것으로 나타났다. 2성분계 전극 중 RhB 제거 성능이 가장 우수하였던 Ru:Sn=9:1 전극에서 4종류의 산화제 생성 농도가 높은 것으로 나타났다. Ru:Pt=9:1 전극은 RhB 분해 성능이 5 전극 중 가장 낮았으며, 산화제도 생성량이 가장 적은 것으로 나타났다. Ru-Sn/Ti 계 전극의 RhB 분해 성능과 산화제 생성 농도가 실험한 모든 1, 2성분계 전극에서 높은 것으로 나타나 향후 3, 4성분계 전극 제조시 이를 바탕으로 제조하고 다른 물질들은 보조재료로서 사용할 필요성이 있는 것으로 사료되었다.

• Applied Biological Chemistry
• /
• v.47 no.3
• /
• pp.332-338
• /
• 2004

An investigation in search of the best oxidizing agent for smoke generators using rice chaff as a combustible carrier was carried out. Smoke rods formulated with active ingredients (AIs) such as inorganic oxidizing agents, glue, and powdered rice chaff, showed constant and high burning rate and high smoking rate on 11 kinds of pesticides. Sodium chlorate was the most suitable oxidizing agent for smoke rod. Even though the sodium chlorate content of the formulation showing the highest smoking rate of AI was variable to pesticides, the smoking rate appeared to increase as the burning rate increased. Active ingredients in smoke generator using rice chaff as a combustible carrier were stable for 60 days when stored at $50^{\circ}C$. An apparatus designed for smoke trapping was useful to collect smoked active ingredients.

• Korean Journal of Food Science and Technology
• /
• v.21 no.4
• /
• pp.468-479
• /
• 1989

The oxidative stability of the ramyon prepared with rapeseed oil fortified with antioxidants or blended with palm oil was studied to explore the possibility of substituting it for Imported frying fats and oils. Natural tocopherols, butylated hydroxyanisole(BHA), tertiarybutyl hydroquinone(TBHQ), and ascorbyl palmitate with citric acid were used at a level of 0.02 percent. Blended oils were prepared by adding a palm oil to the rapeseed oil at ratios of 7:3, 5:5, and 3:7(w/w), respectively. Ramyon samples were stored at $35.0{\pm}0.5^{\circ}C$. for 90 days. The values of parameters, such as peroxide value, unsaturation ratio, and dielectric constant, of the extracted oils were regularly determined. An organoleptic test for the flavor of the samples was also performed. The oxidative stability of the samples was estimated on the basis of the changes of the parameter values. The effectiveness of the antioxidants was in the order of TBHQ ${\gg}$ ascorbyl palmitate with citric acid>BHA>natural tocopherols. The oxidative stability of the ramyon prepared with the rapeseed oil containing 0.02 percent TBHQ was almost as good as that of the ramyon prepared with the palm oil. The stability of the ramyon prepared with the blended oil containing 70 percent palm oil was also as good as that of the ramyon prepared with the palm oil.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.12 no.2
• /
• pp.48-56
• /
• 2008

In the rocket preburner, oxidizer-rich combustion with liquid oxygen and kerosene is very challenging work. The key factor of stable flame is good mixing and that is controlled by the injector performance. We have studied spray characteristics of the oxidizer-rich rocket preburner injector in high pressure environments. The injector is composed of fuel orifices, oxidizer orifices and cooling skirt with liquid oxygen. By using this apparatus, we have taken photographs and measured Sauter mean diameter with changing ambient pressure from 0 to 30 kgf/cm2[g]. Droplet diameter is measured by the image processing technique. From the test results, we could understand spray characteristics of the oxidizer-rich preburner injector and this result could be applied to the development of the oxidizer rich preburner system.

• Journal of the Korean Geotechnical Society
• /
• v.19 no.6
• /
• pp.23-29
• /
• 2003

In this paper, effects of the acidification of ground and the chemical additive materials-ferric oxide, calcium chloride and calcium sulphate on the compressibility characteristics of the marine clay treated with quick lime were investigated. The rapid inflection point method was carried out. Results showed that the compression index of the untreated marine clay increased as the pH of pore water decreased. Also, the preconsolidation pressure, the coefficient of consolidation and the coefficient of permeability of the untreated marine clay decreased with pH of pore water. In the case of the marine clay treated with the quick lime-calcium chloride, the compression index decreased and the coefficient of consolidation and the coefficient of permeability increased. Specially, the preconsolidation pressure of sample treated with the quick lime-ferric oxide was higher than that of another samples.

• Journal of Korean Society of Water and Wastewater
• /
• v.19 no.5
• /
• pp.625-631
• /
• 2005

Disinfection characteristics of mixed oxidants produced by mean of electro-chemical method were evaluated. Inactivation rate of B. subtilis spore on the mixed oxidants were similar with that of chlorine. Based on the experimental results, activation energy of mixed oxidants and chlorine with B. subtilis spore at pH 8.3 were calculated as 30.8, $34.7kJ{\cdot}mol^{-1}$ respectively. UV absorption spectrum of both chlorine and mixed oxidants present similar. Molar extinction coefficients of chlorine and mixed oxidants at 292nm, which is maximum absorption wavelength of $OCl^-$ were 357, $377M^{-1}cm^{-1}$, respectively. Disinfectant decay rate and formation rate of THM in the S WTP filtrate also shows insignificant difference for both mixed oxidants and chlorine. In consequent, it was confirmed that high portion of chlorine presents in the mixed oxidants.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.11 no.4
• /
• pp.46-51
• /
• 2007

The irregular fuel surface was observed by the visualization of hybrid rocket combustion. Even though the test condition maintained oxidizer rich environment, the irregular dark fuel surface was formed as the result of incomplete combustion. In order to investigate the correlation of the characteristics of oxidizer flow and the irregular fuel surface, various flow conditions were imposed such as swirl flow, induced swirl flow by helical fuel configuration and straight flow. Test results revealed no correlation was found between oxidizer flow condition and irregular fuel surface. And this can be a commonly observed phenomena in the tests with different fuel/oxidizer combination. Thus, the irregular fuel surface can be a result of the interaction of blowing flow of vaporized fuel and the boundary layer of oxidizer flow. A further study will be required to confirm the assumption for the formation of irregular fuel surface.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.11 no.4
• /
• pp.52-58
• /
• 2007

The irregular fuel surface was observed by the visualization of hybrid rocket combustion. Even though the test condition maintained oxidizer rich environment, the irregular dark fuel surface was formed as the result of incomplete combustion. In order to investigate the correlation of the characteristics of oxidizer flow and the irregular fuel surface, various flow conditions were imposed such as swirl flow, induced swirl flow by helical fuel configuration and straight flow. Test results revealed no correlation was found between oxidizer flow condition and irregular fuel surface. And this can be a commonly observed phenomena in the tests with different fuel/oxidizer combination. Thus, the irregular fuel surface can be a result of the interaction of blowing flow of vaporized fuel and the boundary layer of oxidizer flow. A further study will be required to confirm the assumption for the formation of irregular fuel surface.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.3 no.3
• /
• pp.1-8
• /
• 1999

Mixing efficiency of the unlike Impinging split triplet injector(FOOF type) were measured to investigate the effect of the momentum ratio variation. $H_2$O/kerosene were used as a propellant simulant. The maximum mixing efficiency occured at the momentum ratio 1.5 (total mixture ratio 1.89). Calculated mixing efficiency of real propellant LOX/Kerosene showed similar trend but maximum efficiency of characteristic velocity occurs at the momentum ratio 2.0(total mixture ratio 2.17). Although there exist a little discrepancy between calculated mixing efficiency based on simulant cold test and hot fire test results, this calculated mixing efficiency can be used to predict hot fire mixing efficiency.