• Proceedings of the KIEE Conference
• /
• 2000.07c
• /
• pp.1800-1802
• /
• 2000

본 연구에서는 냉음극 발광 소자인 FEA를 이용하여 Cold Cathode Lamp 제작과 그 구조에 대해서 연구하였다. Anode plate에는 ZnO:Zn 형광체를 전기영동법으로 증착한 후 tube slabs와 anode plate를 frit glass를 이용하여 접합하였다. FEA와 substrate의 bonding, addressing을 위한 wire bonding, substrate와 집속전극, setter를 stem base의 외부전극에 연결하기 위한 spot welding, tube와 stem base를 glass melting method로 접합 공정을 하였다. 진공배기 시스템에 배기판을 연결하여 ${\sim}10^{-7}$torr까지 배기한 후 heater를 이용하여 배기관을 tip-off하였다. 최종적으로 진공을 유지하기 위해 getter를 RF 고주파로 활성화하였다. 결론적으로 lamp외 특성을 비교분석한 후 휘도 및 발광효율을 향상시키기 위한 구조절 개선과 방안을 고찰하였다.

• Journal of the Korean Institute of Telematics and Electronics
• /
• v.5 no.1
• /
• pp.66-72
• /
• 1968

• Proceedings of the Korean Institute of Communication Sciences Conference
• /
• 1998.10a
• /
• pp.731-735
• /
• 1998

• Proceedings of the Korean Institute of Communication Sciences Conference
• /
• 1993.10a
• /
• pp.341-344
• /
• 1993

• The Magazine of Kiice
• /
• v.4 no.2
• /
• pp.52-57
• /
• 2003

• Journal of Aerospace System Engineering
• /
• v.12 no.5
• /
• pp.8-15
• /
• 2018

The geostationary satellite uses a liquid apogee engine, to obtain a required velocity increment to enter a geostationary orbit. However, as the liquid apogee engine operates in the vacuum, a considerable disbursement of exhaust plume flow, from the liquid apogee engine can trigger a backflow. As this backflow may possibly collide with the satellite directly, it can cause adverse effects such as surface contamination, thermal load, and altitude disturbance, that can generate performance reduction of the geostationary satellite. So, this study investigated exhaust plume behavior of 400 N grade liquid apogee engine numerically. To analyze exhaust plume behavior in vacuum condition, the DSMC (Direct Simulation Monte Carlo) method based on Boltzmann equation is used. As a result, thermal fluid characteristics of exhaust plume such as temperature and number density, are observed.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.47 no.9
• /
• pp.649-657
• /
• 2019

Hydrazine, which is used as a representative monopropellant, is an extremely poisonous substance and has a disadvantage that it is harmful to the human body and is very difficult to handle. In recent years, research on the development of non-toxic and environmentally friendly propellants has attracted much attention. Ammonium dinitramide(ADN) based propellant developed by Swedish Space Corporation has superior performance to hydrazine and has been commercialized through performance verification in space environment. On the other hand, the exhaust gas from a thruster nozzle collides with a satellite while it is spreading in the vacuum space, thermal load and surface contamination may occur and may reduce the performance and lifetime of the satellite. However, a study on the effect of the exhaust gas of the green propellant thruster on the satellite has not been conducted in earnest yet. Therefore, the exhaust gas behavior in space was analyzed in this study for the ADN based green monopropellant using Navier-Stokes equations and the DSMC method. As a result, it can be expected to be used as design validation data in the development of satellite when using the ADN based green monopropellant.

• The Journal of Korean Institute of Communications and Information Sciences
• /
• v.32 no.2A
• /
• pp.213-219
• /
• 2007

In this paper, A novel structure of frequency doubler using Phase Delay line and $90^{\circ}$ Hybrid coupler at harmonic output have been designed and implemented to improve suppression. Proposed structure of frequency doubler improve output. coupling and fundamental suppression. Active frequency doubler with band from $2.13{\sim}2.15GHz\;to\;4.26{\sim}4.3GHz$ was designed and fabricated with 10dBm input power, 0.79dB conversion gain and -55.54dBc suppression at fundamental frequency, -44.76dBc suppression at third harmonic frequency 6.42GHz and -39.18dBc suppression at fourth harmonic frequency 8.56GHz.

• Journal of Nuclear Fuel Cycle and Waste Technology(JNFCWT)
• /
• v.13 no.3
• /
• pp.235-242
• /
• 2015

A commercially available copper mesh was investigated as an iodine off-gas capturing medium for pyroprocessing, with an aim to replace costly silver based adsorbents. Theoretical calculation results suggested that the reaction between metallic copper and gaseous iodine will occur spontaneously to produce copper iodide in the temperature range of 100 ~ 500℃. The effect of the reaction temperature on iodine capturing efficiency was investigated by experimentation, and it was found that 5 and 6 wt% of iodine (initial mass 2.0 g) was captured by a single copper mesh (0.26 g) at 300 and 400℃, respectively. The repeated experimental results also suggested that copper utilization can be increased with the help of the spontaneous detachment of the reaction product (CuI) from a copper mesh. The formation of the CuI phase was confirmed using the X-ray diffraction technique, and the surface morphology of the reaction product was observed using scanning electron microscopy.

• Journal of the Korean Vacuum Society
• /
• v.10 no.2
• /
• pp.164-172
• /
• 2001

We measured the pumpdown curves of an A5083 vacuum chamber and analyzed the outgassing in terms of desorption energies of water. The outgassing curves follow a ~$t^{-1.15}$ behavior before bakeout, which can be described by the first-order desorption of water molecules in the oxide layer. Analysis of the curves reveals that there exist several adsorption sites on the surface for water in the pressure range of ~$10^{-5}\;-\;10^{ -8}$Torr. Measurements utilizing the throughput method show that the room temperature outgassing rate is ~1{\times}10^{-13}$ Torr $\ell$/s $\textrm{cm}^2$ after 24 - h bakeout at $100^{\circ}C$.