THE COSMIC INFRARED BACKGROUND EXPERIMENT (CIBER): A SOUNDING ROCKET PAYLOAD TO STUDY THE NEAR INFRARED EXTRAGALACTIC BACKGROUND LIGHT

被引:29
作者
Zemcov, M. [1 ,2 ]
Arai, T. [3 ,4 ]
Battle, J. [2 ]
Bock, J. [1 ,2 ]
Cooray, A. [5 ]
Hristov, V. [1 ]
Keating, B. [6 ]
Kim, M. G. [7 ]
Lee, D. H. [8 ]
Levenson, L. R. [1 ]
Mason, P. [1 ]
Matsumoto, T. [3 ,7 ]
Matsuura, S. [3 ]
Nam, U. W. [8 ]
Renbarger, T. [6 ]
Sullivan, I. [9 ]
Suzuki, K. [10 ]
Tsumura, K. [3 ]
Wada, T. [3 ]
机构
[1] CALTECH, Dept Phys Math & Astron, Pasadena, CA 91125 USA
[2] NASA, Jet Prop Lab, Pasadena, CA 91109 USA
[3] Japan Aerosp Explorat Agcy JAXA, Dept Space Astron & Astrophys, Inst Space & Astronaut Sci, Sagamihara, Kanagawa 2525210, Japan
[4] Univ Tokyo, Grad Sch Sci, Dept Phys, Tokyo 1130033, Japan
[5] Univ Calif Irvine, Ctr Cosmol, Irvine, CA 92697 USA
[6] Univ Calif San Diego, Dept Phys, San Diego, CA 92093 USA
[7] Seoul Natl Univ, Dept Phys & Astron, Seoul 151742, South Korea
[8] Korea Astron & Space Sci Inst KASI, Taejon 305348, South Korea
[9] Univ Washington, Dept Phys, Seattle, WA 98195 USA
[10] Nagoya Univ, Ctr Tech, Instrument Dev Grp, Nagoya, Aichi 4648602, Japan
关键词
dark ages; reionization; first stars; diffuse radiation; infrared: diffuse background; instrumentation: spectrographs; space vehicles: instruments; zodiacal dust; EMISSION; SEARCH;
D O I
10.1088/0067-0049/207/2/31
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
The Cosmic Infrared Background Experiment (CIBER) is a suite of four instruments designed to study the near infrared (IR) background light from above the Earth's atmosphere. The instrument package comprises two imaging telescopes designed to characterize spatial anisotropy in the extragalactic IR background caused by cosmological structure during the epoch of reionization, a low resolution spectrometer to measure the absolute spectrum of the extragalactic IR background, and a narrow band spectrometer optimized to measure the absolute brightness of the zodiacal light foreground. In this paper we describe the design and characterization of the CIBER payload. The detailed mechanical, cryogenic, and electrical design of the system are presented, including all system components common to the four instruments. We present the methods and equipment used to characterize the instruments before and after flight, and give a detailed description of CIBER's flight profile and configurations. CIBER is designed to be recoverable and has flown four times, with modifications to the payload having been informed by analysis of the first flight data. All four instruments performed to specifications during the subsequent flights, and the scientific data from these flights are currently being analyzed.
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