• 제목/요약/키워드: space telescope mirror

검색결과 80건 처리시간 0.03초

Baffle design and test for wide-field off-axis telescopes

  • 김상혁;박수종;장성혁;김권희;양순철;;허명상;임명신
    • 천문학회보
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    • 제38권1호
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    • pp.72.2-72.2
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    • 2013
  • An off-axis telescope has several advantages in optical performance comparing with a conventional on-axis telescope. However, in general, an off-axis telescope has a narrow field of view due to the linear astigmatism caused by the asymmetric structure. It was shown in the previous work that the linear astigmatism can be eliminated by properly configuring parameters in a confocal off-axis reflector system. Furthermore, the third order aberrations of a confocal off-axis telescope can be minimized by optimizing the shape of the mirrors. Despite many advantages, the confocal off-axis telescopes have been evaded because of difficulties of off-axis mirror fabrication, alignment process and unaccustomed off-axis baffle design. The baffle for the off-axis telescope should be designed considering that the effects of stray lights are different because of the asymmetry of off-axis system. In this poster, the design, manufacturing, and test for the baffle and housing of an off-axis telescope are presented.

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컴퓨터 제작 홀로그램과 데오도라이트를 이용한 인공위성 카메라 주 반사경의 정점 좌표 측정 (Measurement of Primary-mirror Vertex Coordinates for a Space Camera by Using a Computer-generated Hologram and a Theodolite)

  • 강혜은;송재봉;양호순;김학용
    • 한국광학회지
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    • 제28권4호
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    • pp.146-152
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    • 2017
  • 우주용 인공위성 카메라를 구성하는 반사경의 정렬은 광학계의 고분해능, 고성능을 얻기 위한 중요한 과정 중 하나이다. 반사경들의 상호정렬에는 큐브미러(cube mirror)가 대신 사용되기 때문에, 각 반사경과 해당 큐브미러 간의 상호위치관계 정보가 우선 필요하다. 따라서 우주용 카메라 반사경들의 정렬을 위해 각 반사경의 정점과 해당 큐브미러의 상대 좌표값을 정확하게 측정해야하며, 본 논문에서는 컴퓨터 제작 홀로그램(computer-generated hologram, CGH)의 정렬용 세그먼트와 광섬유를 이용하는 새로운 측정 시스템을 제안함으로써 우주용 카메라를 구성하는 반사경의 정점을 요구조건 이내로 측정할 수 있었다. 측정 시스템은 광학계 평가용 간섭계, CGH, 광섬유, 반사경으로 구성되어 있으며, 최종적으로 데오도라이트를 이용해 큐브미러를 기준으로 주 반사경의 정점에 위치한 광섬유 끝단의 3차원 상대 좌표값을 $25{\mu}m$ 이하의 정밀도로 측정할 수 있었다.

Optomechanical Design and Vibration Analysis for Linear Astigmatism-Free Three Mirror System (LAF-TMS)

  • Park, Woojin;Lim, Jae Hyuk;Lee, Sunwoo;Hammar, Arvid;Kim, Sanghyuk;Kim, Yunjong;Jeong, Byeongjoon;Kim, Geon Hee;Chang, Seunghyuk;Pak, Soojong
    • 천문학회보
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    • 제44권2호
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    • pp.47.1-47.1
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    • 2019
  • We report the design and vibration analysis for the optomechanical structures of Linear Astigmatism Free - Three Mirror System (LAF-TMS). LAF-TMS is the linear astigmatism free off-axis wide-field telescope with D = 150 mm, F/3.3, and FOV = 5.51° × 4.13°. The whole structure consists of four optomechanical modules. It can accurately mount mirrors and also can survive from vibration environments. The Mass Acceleration Curve (MAC) is adapted to the quasi-static analysis. Modal, harmonic, and random vibration analysis have been performed under the qualification level of the launch system. We evaluate the final results in terms of von Mises stress and Margin of Safety (MoS).

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KASINICS의 광기계부 설계 (OPTO-MECHANICAL DESIGN OF THE KASINICS)

  • 육인수;이성호;진호;선광일;박수종;이대희;남욱원;문봉곤;차상목;한정열;경재만;김건희;양진석
    • 천문학논총
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    • 제20권1호
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    • pp.143-149
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    • 2005
  • KASI (Korea Astronomy and Space Science Institute) is developing the near-infrared camera system named KASINICS (KASI Near-Infrared Camera System) which will be installed at the 60cm f/13.5 Ritchey-Chretien telescope of the Sobaeksan Optical Astronomy Observatory (SOAO). The camera system is optimized for JHKL bands and has a 6 arcmin FOV. The optical system consists of two spherical mirrors and a 8-position filter wheel. With the exception for the dewar window, all optical elements are cooled inside cryogenic dewar. Since the Offner system is adopted to prevent thermal noises from outside of the telescope primary mirror, the secondary mirror of the Offner system acts as a cold Lyot stop. The optical performance does not change by temperature variations because the Aluminum mirrors contract and expand homogeneously with its mount. We finished the design and fabrication of the optical parts and are now aligning the optical system. We plan to have a test observation on 2006 January.

DESIGN CONSIDERATION FOR HIGH STABILITY TELESCOPE STRUCTURE

  • Lee, Deog-Gyu;Jang, Hong-Sul;Lee, Eung-Shik;Jung, Dae-Jun;Lee, Seung-Hoon
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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    • pp.225-228
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    • 2005
  • Telescope structure based on Korsch type optical layout was suggested for a large aperture optical system. Korsch type optical layout is regarded as providing wide field of view and no color aberration for which high resolution space cameras greatly demand. For the suggested Korsch type telescope structure, two folding mirrors are adopted, firstly to provide for the refocusing device mounting plane on the second fold mirror assembly, secondly by double folding the light path to concisely confine focal plane assembly within the perimeter of the tube. Optical layput design and corresponding support structure design were attained.

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이중 정합법을 이용한 볼록비구면 반사경의 형상 오차 측정 (Surface-error Measurement for a Convex Aspheric Mirror Using a Double-stitching Method)

  • 김고은;이윤우;양호순
    • 한국광학회지
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    • 제32권6호
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    • pp.314-322
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    • 2021
  • 일반적인 반사식 망원경은 오목 형태의 주경과 볼록 형태의 부경으로 구성되어 있다. 주경은 크기가 크지만 빛을 모아주는 특성으로 반사경의 파면오차 측정이 비교적 용이하다. 반면에 부경은 빛을 퍼트리기 때문에 주경보다 크기는 작지만 측정의 난이도는 더 높다고 할 수 있다. 특히 코시(Korsch) 형태의 망원경에서는 부경의 가운데 영역도 사용하는데 기존의 힌들(Hindle) 측정법으로는 가운데 부분을 측정할 수 없다. 본 논문에서는 크기가 큰 볼록비구면을 측정하기 위해 힌들 정합법(힌들 측정법과 정합법의 결합)을 적용하여 측정하고 이 측정에서 빠지는 가운데 영역은 일반간섭계의 구면파를 이용해 측정하여 두 결과를 합쳐 전체 형상 오차를 획득하는 방법을 제안하고자 한다. 제안한 방법으로 직경 202 mm, 곡률 반경 499 mm, 비구면상수 -4.613의 볼록 비구면의 형상 오차를 측정한 결과 19.5±1.3 nm rms로 측정되었다. 이 결과는 상용 정합 측정 장비로 측정한 결과와 0.7 nm rms의 근소한 차이를 보였고 반사경의 형상 오차가 45도 방향 비점수차를 가지는 것것도 일치하였다. 따라서 본 논문에서 제안한 방법이 볼록 비구면의 전체 영역을 정밀하게 측정하는데 유용함을 알 수 있었다.

웨이퍼 레벨 공정이 가능한 2축 수직 콤 구동 방식 마이크로미러 (Wafer-Level Fabrication of a Two-Axis Micromirror Driven by the Vertical Comb Drive)

  • 김민수;유병욱;진주영;전진아;;박재형;김용권
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2007년도 Techno-Fair 및 추계학술대회 논문집 전기물성,응용부문
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    • pp.148-149
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    • 2007
  • We present the design and fabrication prcoess of a two-axis tilting micromirror device driven by the electrostatic vertical comb actuator. A high aspect-ratio comb actuator is fabricated by multiple DRIE process in order to achieve large scan angle. The proposed fabrication process enables a mirror to be fabricated on the wafer-scale. By bonding a double-side polished (DSP) wafer and a silicon-on-insulator (SOI) wafer together, all actuators on the wafer are completely hidden under the reflectors. Nickel lines are embedded on a Pyrex wafer for the electrical access to numerous electrodes of mirrors. An anodic bonding step is implemented to contact electrical lines with ail electrodes on the wafer at a time. The mechanical angle of a fabricated mirror has been measured to be 1.9 degree and 1.6 degree, respectively, in the two orthogonal axes under driving voltages of 100 V. Also, a $8{\times}8$ array of micromirrors with high fill-factor of 70 % is fabricated by the same fabrication process.

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Sensitivity Analysis of the Optical System for UV-IR Space Telescope

  • Kim, Sanghyuk;Chang, Seunghyuk;Pak, Soojong;Jeong, Byeongjoon;Kim, Geon Hee;Hammar, Arvid
    • 천문학회보
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    • 제40권2호
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    • pp.56.4-57
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    • 2015
  • We present the optical design and a sensitivity analysis for a wide field of view (FOV) instrument operating at UV and IR wavelengths. The ongoing investigation is performed in collaboration with Omnisys Instruments (Sweden) and focuses on a telluric-limb-viewing instrument that will fly in a low Earth orbit to study mesospheric wave structures over a wide range of horizontal scales in the altitude range 80 - 100 km. The instrument has six wavelength channels which consist of 4 channels of IR and 2 of UV. We are proposing an optical design based on three mirror aplanatic off-axis reflective system. The entrance pupil diameter and effective focal length are 45 mm and 270 mm, respectively. The FOV is $5.5^{\circ}{\times}1^{\circ}$ and the secondary mirror is set for stop. The optical specification is required to have an encircled energy of at least 80 % within a diameter of 21 um. We performed sensitivity analysis for the longest wavelength of 772 nm in consideration of the diffraction limit of system. The results show that tolerance limits for positions and angles of the mirrors are not very sensitive compared with typical error budgets of manufacturing and assembling process. The secondary mirror has the most sensitive tolerance for surface figure of 250 nm in root-mean-square.

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Assembly Process of FSMP

  • Kim, Jihun;Kim, Young-Soo;Song, Je Heon;Cho, Myung;Park, Won Hyun;Yang, Ho-Soon;Lee, Joohyung;Kim, Ho-Sang;Lee, Chanhee;Lee, Won Gi;Kim, Kyung Il;Lee, Kyoung-Don;Park, Byeong-Gon
    • 천문학회보
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    • 제39권2호
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    • pp.120.1-120.1
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    • 2014
  • Fast-steering Secondary Mirror prototype (FSMP) of the Giant Magellan Telescope (GMT) has been developed by the consortium consisting of institutes in Korea and the US. In 2014 we are finalizing the FSMP project as combining two sub-systems, the mirror fabricated by Korea Research Institute of Standards and Science (KRISS) and the mirror cell with tip-tilt controlling system developed by Institute for Advanced Engineering (IAE), in the KRISS facility. In the assembly process we will identify potential difficulties or problems for the process, such that this process can be reflected to the further development of the FSM for GMT. In the presentation, we present how the assembly process can be carried out in safety.

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A CRYOGENIC TWO MILLIMETER RECEIVER SYSTEM

  • Lee, Chang-Hoon;Han, Seog-Tae;Park, Yong-Sun
    • Journal of Astronomy and Space Sciences
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    • 제11권2호
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    • pp.232-249
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    • 1994
  • Since we finished the purchase of the cooled Schottky diode mixer receiver made by Radiometer Physics Co. for the 120-170GHz range in October 1991, we have not prepared the PPL hardware and software for this receiver and the ellipsolidal mirror for beam guiding. After these problems were solved, this receiver was installed at the 14m telescope in late December 1993, and used for the confirmation of a spectral line detection and the measurement of the beam efficiency. The beam efficiency is about 36% at 146 GHz.

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