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In-Flight Calibration and Performance of the OSIRIS-REx Touch And Go Camera System (TAGCAMS)

Authors :
William M. Owen
K. Getzandanner
L. T. Seals
M. A. Ravine
J. Hikes
D. LeDuc
K. E. Gordon
K. Alkiek
J. N. Kidd
J. Y. Pelgrift
K. Drozd
J. Butt
Brent J. Bos
E. C. A. Church
Arlin E. Bartels
Conor O. Haney
R. Witherspoon
Coralie D. Adam
C. D. Norman
Rajendra Bhatt
Michael Caplinger
Eric M. Sahr
L. R. Chevres-Fernandez
David R. Doelling
Dante S. Lauretta
C. W. May
D. Huish
Andrew J. Liounis
Derek S. Nelson
Michael C. Moreau
Konstantin V. Khlopenkov
A. Wolfram
R. Olds
Source :
Space Science Reviews. 216
Publication Year :
2020
Publisher :
Springer Science and Business Media LLC, 2020.

Abstract

The Touch And Go Camera System (TAGCAMS) is a three-camera-head instrument onboard NASA’s OSIRIS-REx asteroid sample return mission spacecraft. The purpose of TAGCAMS is to facilitate navigation to the target asteroid, (101955) Bennu; confirm acquisition of the asteroid sample; document asteroid sample stowage; and provide supplementary imaging for OSIRIS-REx science investigations. During the almost two-year OSIRIS-REx outbound cruise phase we pursued nine TAGCAMS imaging campaigns to check, calibrate and characterize the camera system’s performance before asteroid arrival and proximity operations began in late 2018. The TAGCAMS in-flight calibration dataset provides the relevant information to enable the three cameras to complete their primary observation goals during asteroid operations. The key performance parameters that we investigated in flight included: linearity, responsivity (both point source and extended body), dark current, hot pixels, pointing, image geometry transformation, image quality and stray light. Analyses of the in-flight performance either confirmed the continued applicability of the TAGCAMS ground test results or substantially improved upon the ground test knowledge. In addition, the TAGCAMS calibration observations identified the source of a spacecraft outgassing feature that guided successful remediation efforts prior to asteroid arrival.

Details

ISSN :
15729672 and 00386308
Volume :
216
Database :
OpenAIRE
Journal :
Space Science Reviews
Accession number :
edsair.doi...........136223691e7393ea8ed8335020e1f092