• 제목/요약/키워드: space instrument

검색결과 482건 처리시간 0.021초

IGRINS Design and Performance Report

  • Park, Chan;Jaffe, Daniel T.;Yuk, In-Soo;Chun, Moo-Young;Pak, Soojong;Kim, Kang-Min;Pavel, Michael;Lee, Hanshin;Oh, Heeyoung;Jeong, Ueejeong;Sim, Chae Kyung;Lee, Hye-In;Le, Huynh Anh Nguyen;Strubhar, Joseph;Gully-Santiago, Michael;Oh, Jae Sok;Cha, Sang-Mok;Moon, Bongkon;Park, Kwijong;Brooks, Cynthia;Ko, Kyeongyeon;Han, Jeong-Yeol;Nah, Jakyuong;Hill, Peter C.;Lee, Sungho;Barnes, Stuart;Yu, Young Sam;Kaplan, Kyle;Mace, Gregory;Kim, Hwihyun;Lee, Jae-Joon;Hwang, Narae;Kang, Wonseok;Park, Byeong-Gon
    • 천문학회보
    • /
    • 제39권2호
    • /
    • pp.90-90
    • /
    • 2014
  • The Immersion Grating Infrared Spectrometer (IGRINS) is the first astronomical spectrograph that uses a silicon immersion grating as its dispersive element. IGRINS fully covers the H and K band atmospheric transmission windows in a single exposure. It is a compact high-resolution cross-dispersion spectrometer whose resolving power R is 40,000. An individual volume phase holographic grating serves as a secondary dispersing element for each of the H and K spectrograph arms. On the 2.7m Harlan J. Smith telescope at the McDonald Observatory, the slit size is $1^{{\prime}{\prime}}{\times}15^{{\prime}{\prime}}$. IGRINS has a plate scale of 0.27" pixel-1 on a $2048{\times}2048$ pixel Teledyne Scientific & Imaging HAWAII-2RG detector with a SIDECAR ASIC cryogenic controller. The instrument includes four subsystems; a calibration unit, an input relay optics module, a slit-viewing camera, and nearly identical H and K spectrograph modules. The use of a silicon immersion grating and a compact white pupil design allows the spectrograph collimated beam size to be 25mm, which permits the entire cryogenic system to be contained in a moderately sized ($0.96m{\times}0.6m{\times}0.38m$) rectangular Dewar. The fabrication and assembly of the optical and mechanical components were completed in 2013. From January to July of this year, we completed the system optical alignment and carried out commissioning observations on three runs to improve the efficiency of the instrument software and hardware. We describe the major design characteristics of the instrument including the system requirements and the technical strategy to meet them. We also present the instrumental performance test results derived from the commissioning runs at the McDonald Observatory.

  • PDF

Observations of Solar Filaments with Fast Imaging Solar Spectrograph of the 1.6 meter New Solar Telescope at Big Bear Solar Observatory

  • Song, Dong-Uk;Park, Hyung-Min;Chae, Jong-Chul;Yang, Hee-Su;Park, Young-Deuk;Nah, Ja-Kyoung;Cho, Kyung-Suk;Jang, Bi-Ho;Ahn, Kwang-Su;Cao, Wenda;Goode, Philip R.
    • 천문학회보
    • /
    • 제36권2호
    • /
    • pp.88.2-88.2
    • /
    • 2011
  • Fast Imaging Solar Spectrograph (FISS) is an instrument developed by Seoul National University and Korea Astronomy and Space Science Institute and installed at the 1.6 meter New Solar Telescope of Big Bear Solar Observatory. Using this instrument, we observed solar filaments and analyzed the data focusing on determining the temperature and non-thermal velocity. We inferred the Doppler absorption widths of $H{\alpha}$ and Ca II 8542$\bar{A}$ lines from the line profiles using the cloud model. From these values, we separately determined temperature and non-thermal velocity. Our first result came from a solar filament observed on 2010 July 29th. Temperature inside a small selected region of this ranges from 4500K to 12000K and non-thermal velocity, from 3.5km/s to 7km/s. We also found temperature varied a lot with time. For example temperature at a fixed point varied from 8000K to 18000K for 40 minutes, displaying an oscillating pattern with a period of about 8 minutes and amplitude of about 2000K. We will also present new results from filaments observed in 2011 summer.

  • PDF

CAPABILITY OF THE FAST IMAGING SOLAR SPECTROGRAPH ON NST/BBSO FOR OBSERVING FILAMENTS/PROMINENCES AT THE SPECTRAL LINES Hα, Ca II 8542, AND Ca II K

  • Ahn, Kwang-Su;Chae, Jong-Chul;Park, Hyung-Min;Nah, Jak-Young;Park, Young-Deuk;Jang, Bi-Ho;Moon, Yong-Jae
    • 천문학회지
    • /
    • 제41권2호
    • /
    • pp.39-47
    • /
    • 2008
  • Spectral line profiles of filaments/prominences to be observed by the Fast Imaging Solar Spectrograph (FISS) are studied. The main spectral lines of interests are $H{\alpha}$, Ca II 8542, and Ca II K. FISS has a high spectral resolving power of $2{\times}10^5$, and supports simultaneous dual-band recording. This instrument will be installed at the 1.6m New Solar Telescope (NST) of Big Bear Solar Observatory, which has a high spatial resolution of 0.065" at 500nm. Adopting the cloud model of radiative transfer and using the model parameters inferred from pre-existing observations, we have simulated a set of spectral profiles of the lines that are emitted by a filament on the disk or a prominence at the limb. Taking into account the parameters of the instrument, we have estimated the photon count to be recorded by the CCD cameras, the signal-to-noise ratios, and so on. We have also found that FISS is suitable for the study of multi-velocity threads in filaments if the spectral profiles of Ca II lines are recorded together with $H{\alpha}$ lines.

Science Objectives and Design of Ionospheric Monitoring Instrument Ionospheric Anomaly Monitoring by Magnetometer And Plasma-probe (IAMMAP) for the CAS500-3 Satellite

  • Ryu, Kwangsun;Lee, Seunguk;Woo, Chang Ho;Lee, Junchan;Jang, Eunjin;Hwang, Jaemin;Kim, Jin-Kyu;Cha, Wonho;Kim, Dong-guk;Koo, BonJu;Park, SeongOg;Choi, Dooyoung;Choi, Cheong Rim
    • Journal of Astronomy and Space Sciences
    • /
    • 제39권3호
    • /
    • pp.117-126
    • /
    • 2022
  • The Ionospheric Anomaly Monitoring by Magnetometer And Plasma-probe (IAMMAP) is one of the scientific instruments for the Compact Advanced Satellite 500-3 (CAS 500-3) which is planned to be launched by Korean Space Launch Vehicle in 2024. The main scientific objective of IAMMAP is to understand the complicated correlation between the equatorial electro-jet (EEJ) and the equatorial ionization anomaly (EIA) which play important roles in the dynamics of the ionospheric plasma in the dayside equator region. IAMMAP consists of an impedance probe (IP) for precise plasma measurement and magnetometers for EEJ current estimation. The designated sun-synchronous orbit along the quasi-meridional plane makes the instrument suitable for studying the EIA and EEJ. The newly-devised IP is expected to obtain the electron density of the ionosphere with unprecedented precision by measuring the upper-hybrid frequency (fUHR) of the ionospheric plasma, which is not affected by the satellite geometry, the spacecraft potential, or contamination unlike conventional Langmuir probes. A set of temperature-tolerant precision fluxgate magnetometers, called Adaptive In-phase MAGnetometer, is employed also for studying the complicated current system in the ionosphere and magnetosphere, which is particularly related with the EEJ caused by the potential difference along the zonal direction.

창의 천문기기 개발 및 관측 교육 프로그램: 소형 분광기 개발 (Creative Education Program of Astronomical Instrument Design and Observation: Development of the Small Spectrograph)

  • 양희수;정종균
    • 우주기술과 응용
    • /
    • 제4권2호
    • /
    • pp.105-120
    • /
    • 2024
  • 현대 천문학에서의 대형 기기 개발은 많은 자원과 인력이 소모되기 때문에 시스템 엔지니어링 및 프로젝트 관리 능력은 현장에서 필수적인 역량이다. 우리는 관측 가능한 실습용 분광기를 제작하고 관측하여 시스템 엔지니어링 경험을 쌓을 수 있는 학부 교육프로그램을 제안한다. 한국천문연구원의 우주인력양성사업의 일환으로 충남대에서 진행된 파일럿 프로그램은 '창의천문기기 개발 및 관측'이라는 가칭으로 총 24명의 학생들이 수강하였으며, 5개 조에서 분광기를 만들어 태양, 달, 별 등의 스펙트럼을 측정하고 연구를 진행하였다. 학생들의 기기 개발과정은 수차례의 리뷰회의를 통하여 가이드 되었으며 개발과정과 문서화된 결과를 통해 성적을 배분하였다. 기기개발 학생들은 이 기회를 통해 시스템 엔지니어링의 기본 원리뿐 아니라 프로젝트 매니지먼트, 광학설계, 기계설계 등에 대해 전반적으로 익힐 수 있었다.

COronal Diagnostic EXperiment (CODEX)

  • Bong, Su-Chan;Kim, Yeon-Han;Choi, Seonghwan;Cho, Kyung-Suk;Newmark, Jeffrey S;Gopalswamy, Natchimuthuk;Gong, Qian;Reginald, Nelson L.;Cyr, Orville Chris St.;Viall, Nicholeen M.;Yashiro, Seiji;Thompson, Linda D.;Strachan, Leonard
    • 천문학회보
    • /
    • 제44권1호
    • /
    • pp.82.2-82.3
    • /
    • 2019
  • Korea Astronomy and Space Science Institute (KASI), in collaboration with the NASA Goddard Sparce Flight Center (GSFC), will develop a next generation coronagraph for the International Space Station (ISS). COronal Diagnostic EXperiment (CODEX) uses multiple filters to obtain simultaneous measurements of electron density, temperature, and velocity within a single instrument. CODEX's regular, systematic, comprehensive dataset will test theories of solar wind acceleration and source, as well as serve to validate and enable improvement of space-weather/operational models in the crucial source region of the solar wind. CODEX subsystems include the coronagraph, pointing system, command and data handling (C&DH) electronics, and power distribution unit. CODEX is integrated onto a standard interface which provides power and communication. All full resolution images are telemeters to the ground, where data from multiple images and sequences are co-added, spatially binned, and ratioed as needed for analysis.

  • PDF

The Dual-Channel, Pulse-Counting Pierce-Blitzstein Photometer-The PBPHOT: Our Last Paper with Bob Koch, and Additional Technical History

  • Ambruster, Carol;Hull, Tony;Koch, Robert H.;Mitchell, Rich;Wolf, George;Smith, Bob
    • Journal of Astronomy and Space Sciences
    • /
    • 제29권2호
    • /
    • pp.195-198
    • /
    • 2012
  • The dual channel Pierce-Blitzstein photometer (PBPHOT) was productively used at the Flower and Cook Observatory to provide 60 years of study of binary systems and other cosmic objects. We review the history of this instrument, discuss its calibration, and recall some personal and professional interactions with Professor Robert H. Koch.

국제우주정거장 범용 데이터인터페이스 시뮬레이터 소프트웨어 상세설계 및 검증 (GUI Design and Realization of Universal Data Interface Simulator for International Space Station)

  • 서석배;김종우;최해진
    • 대한전자공학회:학술대회논문집
    • /
    • 대한전자공학회 2003년도 통신소사이어티 추계학술대회논문집
    • /
    • pp.374-377
    • /
    • 2003
  • ISS UDIS (International Sapce Station Universal Data Interface simulator) is a data communication interface simulator between ISS and instrument. This paper explains design concept, and verifies operations of ISS UDIS simulator. By realization of the simulator, we ensure data interface skills for a manned-space data communication system.

  • PDF