• Title/Summary/Keyword: 탑재시험체

Search Result 247, Processing Time 0.023 seconds

Characteristics of Ocean Scanning Multi-spectral Imager(OSMI) (Ocean Scanning Multi-spectral Imager (OSMI) 특성)

  • Young Min Cho;Sang-Soon Yong;Sun Hee Woo;Sang-Gyu Lee;Kyoung-Hwan Oh;Hong-Yul Paik
    • Korean Journal of Remote Sensing
    • /
    • v.14 no.3
    • /
    • pp.223-231
    • /
    • 1998
  • Ocean Scanning Multispectral Imager (OSMI) is a payload on the Korean Multi-Purpose SATellite (KOMPSAT) to perform worldwide ocean color monitoring for the study of biological oceanography. The instrument images the ocean surface using a whisk-broom motion with a swath width of 800 km and a ground sample distance (GSD) of less than 1 km over the entire field-of-view (FOV). The instrument is designed to have an on-orbit operation duty cycle of 20% over the mission lifetime of 3 years with the functions of programmable gain/offset and on-orbit image data storage. The instrument also performs sun calibration and dark calibration for on-orbit instalment calibration. The OSMI instrument is a multi-spectral imager covering the spectral range from 400 nm to 900 nm using a Charge Coupled Device (CCD) Focal Plane Array (FPA). The ocean colors are monitored using 6 spectral channels that can be selected via ground commands after launch. The instrument performances are fully measured for 8 basic spectral bands centered at 412, 443, 490, 510, 555, 670, 765 and 865 nm during ground characterization of instalment. In addition to the ground calibration, the on-orbit calibration will also be used for the on-orbit band selection. The on-orbit band selection capability can provide great flexibility in ocean color monitoring.

Effects of Dropwort Powder on the Quality of Castella (미나리가루의 첨가가 Castella의 품질에 미치는 영향)

  • Park, Sang-Jun;Lee, Kwang-Suck;An, Bye-Lyung
    • Journal of the East Asian Society of Dietary Life
    • /
    • v.17 no.6
    • /
    • pp.834-839
    • /
    • 2007
  • This study was designed to determine the optimal ratio of dropwort powder in castella by adding the powder at levels of 0, 3, 6, 9, and 12% respectively. The properties of the castella were analyzed by specific gravity, specific volume, color determinations, texture properties and sensory evaluation. The Specific gravity increased with increasing amount of dropwort powder. However, the specific volume decreased with increasing dropwort powder. For the color values, as more dropwort powder was added, the L-value decreased. The castella with 9% dropwort powder had a higher hardness, gumminess, and chewiness. A sensory panel perceived that the external and internal color of the castella become darker with the dropwort powder substitution and the grain size decreased with increasing amount dropwort powder, while sweet taste showed no significant difference. The order of overall preference was DP 9>DP 6>DP 12>CON>DP 3. Therefore, the substitution of 9% of wheat flour with dropwort powder was recommended in the production of castella.

  • PDF

Development and Validation of Cryopanel Cooling System Using Liquid Helium for a Satellite Test (액체헬륨을 이용한 위성시험용 극저온패널 냉각시스템 개발 및 검증)

  • Cho, Hyok-Jin;Moon, Guee-Won;Seo, Hee-Jun;Lee, Sang-Hoon;Hong, Seok-Jong;Choi, Seok-Weon
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.34 no.2
    • /
    • pp.213-218
    • /
    • 2010
  • A cooling system utilizing liquid helium to chill the cryopanel (800 mm $\times$ 700 mm dimensions) down to 4.2 K was designed, implemented, and tested to verify the role of the cryopanel as a heat sink for the payload of a spacecraft inside the large thermal vacuum chamber (effective dimensions : 8 m ($\Phi$) $\times$ 10 m (L)) of KARI (Korea Aerospace Research Institute). Two LHe (Liquid Helium) Dewars, one for the main supply and the other for refilling, were used to supply liquid helium or cold helium gas into this cryopanel, and flow control for the target temperature of the cryopanel within requirements was done through fine adjustment of the pressure inside the LHe Dewars. The return helium gas from the cryopanel was reused as a thermal barrier to minimize the heat influx on the core liquid helium supply pipe. The test verified a cooling time of around three hours from the ambient temperature to 40 K (combined standard uncertainty of 194 mK), the capacity for maintaining the cryopanel at intermediate temperatures, and a 1 K uniformity over the entire cryopanel surface at around 40 K with 20 W cooling power.

Measurement of Vertical-Directional DTV Signal Level Using a Multi-Copter (멀티콥터를 이용한 수직방향 DTV 신호 레벨 측정)

  • Park, Hyung-Do;Lim, Sol;Kim, Dae Jin
    • Journal of Broadcast Engineering
    • /
    • v.19 no.3
    • /
    • pp.372-384
    • /
    • 2014
  • DTV field tests have been performed to measure field strength and to check reception ratio on indoor and outdoor sites. They use an antenna of 9m to measure DTV signal in case of outdoor measurement on the road. Modern skyscrapers require the analysis of vertical-directional wave propagation by measuring vertical-directional DTV signal. Even if the field strength is above the reception threshold of $43dB{\mu}V/m$, the reception is impossible in case of strong multi-path or high impulse noise. So, vertical-directional field measurement is essential in environment of tall buildings. In this paper, we developed an octo type multi-copter to measure vertical-directional DTV signal level. A compact and portable DTV signal level meter, an antenna, a microwave transmitter for data transmission, and a recording equipment are equipped in the multi-copter. Three different sites are selected to test the measurement system. Developed measurement system using the multi-copter is very useful in measuring vertical-directional DTV signal, especially in apartments, non-accessible area by vehicles, and forbidden areas.

Characteristics of Beam-tilting Slot Array Waveguide Antennas for DBS Reception (DBS 수신용 빔 틸트형 슬롯 어레이 도파관 안테나의 특성)

  • Min, Gyeong-Sik;Kim, Dong-Cheol;Arai, Hiroyuki
    • Journal of the Institute of Electronics Engineers of Korea TC
    • /
    • v.39 no.3
    • /
    • pp.140-149
    • /
    • 2002
  • This paper describes the characteristics of beam-tilting slot away waveguide antennas for mobile DBS reception. As a basic study of slotted waveguide array, design for 16 slot elements located on a broad-wall waveguide is considered. Design parameters such as slot length, space between each slot and cross slot angle of antennas with the beam-tilting characteristics are calculated by method of moments. Based on these results, the radiation waveguide antennas with 16-element $\times$16-array are designed and fabricated. The measured main beam direction angles of the fabricated antennas are 48$^{\circ}$to 50$^{\circ}$depending on the measured frequencies and it shows good agreement with prediction. The measured 3 dB beam width of elevation pattern is about 13$^{\circ}$, and the axial ratio and the gain measured at DBS band are observed 2.8 dB below and 24 dBi above, respectively. In order to evaluate a performance of the fabricated waveguide planar antenna, it is combined with the satellite tracking control system and the field performance test of antenna mounted on a mobile vehicle is carried out at highway. During the measurement, it was possible to watch television without a break signal in a driving vehicle and an excellent performance of the proposed antennas was demonstrated.

A Study on the Analysis of Visibility between a Lunar Orbiter and Ground Stations for Trans-Lunar Trajectory and Mission Orbit (지구-달 전이궤적 및 임무 궤도에서 궤도선과 지상국의 가시성 분석에 관한 연구)

  • Choi, Su-Jin;Kim, In-Kyu;Moon, Sang-Man;Kim, Changkyoon;Rew, Dong-young
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.44 no.3
    • /
    • pp.218-227
    • /
    • 2016
  • Korean government plans to launch a lunar orbiter and a lander to the Moon by 2020. Before launch these two proves, an experimental lunar orbiter will be launched by 2018 to obtain key space technologies for the lunar exploration. Several payloads equipped in experimental lunar orbiter will monitor the surface of the Moon and will gather science data. Lunar orbiter sends telemetry and receives tele-command from ground using S-band while science data is sent to ground stations using X-band when the visibility is available. Korean deep space network will be mainly used for S and X-band communication with lunar orbiter. Deep Space Network or Universal Space Network can also be used for the S-band during trans-lunar phase when korean deep space network is not available and will be used for the S-band in normal mission orbit as a backup. This paper analyzes a visibility condition based on the combination of various ground antennas and its mask angles according to mission scenario to predict the number of contacts per day and to build an operational scenario for the lunar orbiter.

Characteristics of the Electro-Optical Camera(EOC) (다목적실용위성탑재 전자광학카메라(EOC)의 성능 특성)

  • Seunghoon Lee;Hyung-Sik Shim;Hong-Yul Paik
    • Korean Journal of Remote Sensing
    • /
    • v.14 no.3
    • /
    • pp.213-222
    • /
    • 1998
  • Electro-Optical Camera(EOC) is the main payload of the KOrea Multi-Purpose SATellite(KOMPSAT) with the mission of cartography to build up a digital map of Korean territory including a Digital Terrain Elevation Map(DTEM). This instalment which comprises EOC Sensor Assembly and EOC Electronics Assembly produces the panchromatic images of 6.6 m GSD with a swath wider than 17 km by push-broom scanning and spacecraft body pointing in a visible range of wavelength, 510~730 nm. The high resolution panchromatic image is to be collected for 2 minutes during 98 minutes of orbit cycle covering about 800 km along ground track, over the mission lifetime of 3 years with the functions of programmable gain/offset and on-board image data storage. The image of 8 bit digitization, which is collected by a full reflective type F8.3 triplet without obscuration, is to be transmitted to Ground Station at a rate less than 25 Mbps. EOC was elaborated to have the performance which meets or surpasses its requirements of design phase. The spectral response, the modulation transfer function, and the uniformity of all the 2592 pixel of CCD of EOC are illustrated as they were measured for the convenience of end-user. The spectral response was measured with respect to each gain setup of EOC and this is expected to give the capability of generating more accurate panchromatic image to the users of EOC data. The modulation transfer function of EOC was measured as greater than 16 % at Nyquist frequency over the entire field of view, which exceeds its requirement of larger than 10 %. The uniformity that shows the relative response of each pixel of CCD was measured at every pixel of the Focal Plane Array of EOC and is illustrated for the data processing.