2025ApJS..280...66Z


Query : 2025ApJS..280...66Z

2025ApJS..280...66Z - Astrophys. J., Suppl. Ser., 280, 66 (2025/October-0)

The Cosmic Infrared Background Experiment-2: An Intensity-mapping Optimized Sounding-rocket Payload to Understand the Near-IR Extragalactic Background Light.

ZEMCOV M., BOCK J.J., COORAY A., MATSUURA S., LEE D.-H., FAZAR C., FEDER R.M., HEATON G., HASHIMOTO R., KORNGUT P., MATSUMOTO T., NGUYEN C.H., NODA K., PARK W.-K., SANO K., TAKIMOTO K., ARAI T., BANG S.-C., BANGALE P., FURUTANI M., HRISTOV V., KAWANO Y., KIDA A., KOJIMA T., LANZ A., MATSUMI C., MERCADO D., NAKAGAWA S., NAKAGAWA T., NAKAHATA S., OHTA R., PATRU D., SHIRAHATA M., SUZUKI H., TAKAHASHI A., TAMAI M., TRAMM S., TSUMURA K., YAMADA Y. and WANG S.-Y.

Abstract (from CDS):

The background light produced by emission from all sources over cosmic history is a powerful diagnostic of structure formation and evolution. At near-infrared wavelengths, this extragalactic background light (EBL) is comprised of emission from galaxies stretching all the way back to the first-light objects present during the Epoch of Reionization. The Cosmic Infrared Background Experiment 2 (CIBER-2) is a sounding-rocket experiment designed to measure both the absolute photometric brightness of the EBL over 0.5-2.0 μm and perform an intensity-mapping measurement of EBL spatial fluctuations in six broad bands over the same wavelength range. CIBER-2 comprises a 28.5 cm, 80 K telescope that images several square degrees to three separate cameras. Each camera is equipped with an HAWAII-2RG detector covered by an assembly that combines two broadband filters and a linear-variable filter, which perform the intensity mapping and absolute photometric measurements, respectively. CIBER-2 has flown three times: an engineering flight in 2021, a terminated launch in 2023, and a successful science flight in 2024. In this paper, we review the science case for the experiment; describe the factors motivating the instrument design; review the optical, mechanical, and electronic implementation of the instrument; present preflight laboratory characterization measurements; and finally assess the instrument's performance in flight.

Abstract Copyright: © 2025. The Author(s). Published by the American Astronomical Society.

Journal keyword(s): Astronomical instrumentation - Infrared telescopes - Rockets - Cosmic background radiation

Simbad objects: 5

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Number of rows : 5
N Identifier Otype ICRS (J2000)
RA
ICRS (J2000)
DEC
Mag U Mag B Mag V Mag R Mag I Sp type #ref
1850 - 2026
#notes
1 NAME COSMOS Field reg 10 00 28.60 +02 12 21.0           ~ 3639 0
2 NAME Lockman Hole reg 10 45 00.0 +58 00 00           ~ 910 0
3 NAME NOAO Deep Wide Field reg 14 32 05.75 +34 16 47.5           ~ 430 0
4 ELAIS N1 reg 16 10 01 +54 30.6           ~ 489 0
5 NAME NEP reg 18 00 00.000 +66 33 38.55           ~ 430 0

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