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1984년 ~ 2025년까지 1,252 건의 한국우주과학회지를 계간으로 확인하실 수 있습니다.
- The Korean Space Science Society (The Korean Astronomical Society)
- 계간 (Quarterly)
- ISSN : 1225-052x (ISSN : 1225-052x)
1225-052x
- DB구축현황 : 1,252건 (DB Construction : 1,252 Articles)
총 게시글 1,252건
페이지 93/126
921
- Kim, Hyo-Min
- 韓國宇宙科學會誌 = Journal of astronomy & space sciences
- 17, n.2
- pp.317-328
- 2000
- 원문 바로보기
The solar wind contributes to the formation of unique space environment called the Earth's magnetosphere by various interactions with the Earth's magnetic field. Thus the solar-terrestrial environment affects the Earth's magnetic field, which can be observed with an instrument for the magnetic field measurement, the magnetometer usually mounted on the rocket and the satellite and based on the ground observatory. The magnetometer is a useful instrument for the spacecraft attitude control as well as the Earth's magnetic field measurements for the spacecraft purpose. In this paper, we present the preliminary design and test results of the two onboard magnetometers of KARI's (Korea Aerospace Research Institute) sounding rocket, KSR-3, which will be launched four times during the period of 2001-02. The KSR-3 magnetometers consist of the fluxgate magnetometer, MAG/AIM (Attitude Information Magnetometer) for acquiring the rocket flight attitude information, and of the search-coil magnetometer, MAG/SIM (Scientific Investigation Magnetometer) for the observation of the Earth's magnetic field fluctuations. With the MAG/AIM, the 3-axis attitude information can be acquired by the comparison of the resulting dc magnetic vector field with the IGRF (International Geomagnetic Reference Field). The Earth's magnetic field fluctuations ranging from 10 to 1,000 Hz can also be observed with the MAG/SIM measurement.
922
- Lee, Byoung-Sun
- 韓國宇宙科學會誌 = Journal of astronomy & space sciences
- 17, n.2
- pp.285-294
- 2000
- 원문 바로보기
The post-launch mission analysis of the KOMPSAT-1 spacecraft was carried out. The injection accuracy of the Taurus launch vehicle was analyzed by comparison of the target and the realized orbit parameters. The tracking station contact analysis was also performed based on the state vectors applied at the day of launch. The offset angles between the predicted orbit and realized orbit were calculated for various tracking stations. The injection orbit parameters of the KOMPSAT-1 were analyzed for the possible options in Launch and Early Orbit Phase(LEOP) operations. Variations of the Local Time of Ascending Node(LTAN) were also obtained.
923
- Sohn, Young-Jong
- 韓國宇宙科學會誌 = Journal of astronomy & space sciences
- 17, n.2
- pp.133-140
- 2000
- 원문 바로보기
From the VI images of M13, obtained by using 2K CCD camera and the BOAO 1.8m telescope, we derive the(V - I) - V CMD of M13. From the shapes of red giant branch, the magnitude of horizontal branch, and the giant branch bump on the constructed CMD, we determined the metallicity of the globular cluster to be 1.74<TEX>${\lesssim}$</TEX>[Fe/H]<TEX>${\lesssim}$</TEX>-1.41. The good agreement between our determination of [Fe/H] and those determined by using other methods implies that the morphology of red giant and horizontal branches on (V - I) - V CMD's can be good indirect metallicity indicators of Galactic globular clusters.
924
- 유광선
- 韓國宇宙科學會誌 = Journal of astronomy & space sciences
- 17, n.1
- pp.67-76
- 2000
- 원문 바로보기
2002년에 발사 예정인 과학 위성 1호의 주 탑재체로 원자외선 분광기가 실릴 예정이다. 원자외선 분광기는 영상과 함께 분광의 기능을 함께 수행을 하게 되는데, 이를 위해 광학적인 요소로서 포물 원통 반사경, 슬릿, 타원형 회절 반사경, 그리고 MCP가 사용된다. 천문학적 관측 목표의 달성을 위한 각 광학 요소의 생산 오차와 위치 오차의 허용 한계를 구하였으며, 이 과정에서 도식적 단순화를 통해 민감도표를 해석하여 각 광학 요소의 조작 범위와 정밀도 등을 구하였다. 선형 오차의 경우 <TEX>$15{\mu}m$</TEX>, 각 오차의 경우 2' 이내의 정밀도로 광학적 요구 조건을 만족할 수 있을 것이다.
925
- 강봉석
- 韓國宇宙科學會誌 = Journal of astronomy & space sciences
- 17, n.1
- pp.19-32
- 2000
- 원문 바로보기
접촉쌍성 VW Cep의 BV 측광관측을 1999년 4-5월 중 7일간 소백산천문대에서 수행하여 총 1,018개의 관측점을 얻었다. 이 관측 자료를 사용하여 광도곡선을 만들었고 이로부터 극심시각 HJD2454327.2282을 결정하였다. 우리의 광도곡선을 Wilson-Devinney 프로그램을 사용하여 분석하였다. 이때 모드 3을 적용하였고, <TEX>$i,T_2,\Omega_1,q,L_1$</TEX>을 수정인자로, 나머지 요소는 모두 고정인자로 사용하였다. WD 프로그램 초기 입력값으로 <TEX>$T_1,a,V_r$</TEX>은 Kaszas et al. (1998)의 값을, A는 Hendry et al. (1992)의 값을, X1는 van Hamme (1993)의 값을 사용하였다. 우리의 광도곡선해와 Kaszas et al. (1998)의 분광학적 해를 결합하여 VW Cep의 절대량<TEX>$M_1=0.95M_\odot,M_2=0.33M_\odot,R_1=1.02R_\odot,R_2=0.66R_\odot$</TEX>을 산출했다.
926
- 이동한
- 韓國宇宙科學會誌 = Journal of astronomy & space sciences
- 17, n.2
- pp.295-308
- 2000
- 원문 바로보기
OSMI(Ocean Scanning Multi-Spectral Imager) raw image data(Level 0) were acquired and radiometrically corrected. We have applied two methods, using solar & dark calibration data from OSMI sensor and comparing with the SeaWiFS data, to the radiometric correction of OSMI raw image data. First, we could get the values of the gain and the offset for each pixel and each band from comparing the solar & dark calibration data with the solar input radiance values, calculated from the transmittance, BRDF (Bidirectional Reflectance Distribution Function) and the solar incidence angle(<TEX>$\beta$</TEX>, <TEX>$\theta$</TEX>) of OSMI sensor. Applying this calibration data to OSMI raw image data, we got the two odd results, the lower value of the radiometric corrected image data than the expected value, and the Venetian Blind Effect in the radiometric corrected image data. Second, we could get the reasonable results from comparing OSMI raw image data with the SeaWiFS data, and get a new problem of OSMI sensor.
927
- Eun, Jeong-Won
- 韓國宇宙科學會誌 = Journal of astronomy & space sciences
- 17, n.2
- pp.249-256
- 2000
- 원문 바로보기
It has been developed to calculate fuel budget for a geostationary communication and broadcasting satellite. It is quite essential that the pre-launch fuel budget estimation must account for the deterministic transfer and drift orbit maneuver requirements. After on-station, the calculation of satellite lifetime should be based on the estimation of remaining fuel and assessment of actual performance. These estimations step from the proper algorithms to produce the prediction of satellite lifetime. This paper concentrates on the fuel estimation method that was studied for calculation of the propellant budget by using the given algorithms. Applications of this method are discussed for a communication and broadcasting satellite.
928
- Chung, Tae-Jin
- 韓國宇宙科學會誌 = Journal of astronomy & space sciences
- 17, n.2
- pp.257-266
- 2000
- 원문 바로보기
A satellite RF communication link is analyzed based on a simple fundamental equations by systematic approach in this paper. The number of variables related to a design and analysis of satellite RF link is often a dozen or more, thus it is a tedious and time-consuming task. With the given input data, the important parameters are calculated step by step and three communication characteristics such as communication channel capacity, carrier-to-noise ratio(CNR) at the satellite and ground station are analyzed. It gives very useful information to the system engineers for designing and analyzing the overall satellite communication system in the conceptual design phase.
929
- Chung, Jong-Kyun
- 韓國宇宙科學會誌 = Journal of astronomy & space sciences
- 17, n.2
- pp.241-248
- 2000
- 원문 바로보기
A groung Fabry-Perot interferometer has been used to measure atomic oxygen nightglow (OI 630.0nm) from the thermosphere (about 250km) at King Sejong station (KSS, geographic: <TEX>$62.22^{\circ}$</TEX>S, <TEX>$301.25^{\circ}$</TEX>E; geomagnetic: <TEX>$50.65^{\circ}$</TEX>S, <TEX>$7.51^{\circ}$</TEX>E), Antarctica. While numerous studies of the thermosphere have been performed on high latitude using ground-based Fabry-Perot interferometers, the thermospheric measurements in the Southern Hemisphere are relatively new and sparse. Therefore, the nightglow measurements at KSS play an important role in extending the thermospheric studies to the Southern Hemisphere. In this study, we investigated the effects of the geomagnetic and solar activities on the thermospheric neutral temperatures that have been observed at KSS in 1989 and 1997. The measured average temperatures are 1400K in 1989 and 800K in 1997, reflecting the influence of the solar activity. The measurements were compared with empirical models, MSIS-86 and semi-empirical model, VSH.
930
- Kim, Sang-Joon
- 韓國宇宙科學會誌 = Journal of astronomy & space sciences
- 17, n.2
- pp.147-150
- 2000
- 원문 바로보기
A fluorescent equilibrium model for the 1-0 band of the A-X system of <TEX>${18}^{OH}$</TEX> has been constructed. Line positions and intensities have been calculated for possible future spectroscopic observations of these bands from space in order to derive <TEX>${18}^{O}/{16}^{O}$</TEX> ratios in comets. It is demonstrated that the strong lines of the 1-0 band can be observable for a moderately bright comet using a high resolution spectrometer with a reasonable exposure time.