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Table 3 Sensitivity factors at the reference temperature (TCCD, T = − 30 °C), and errors for the band ratios from stellar observations

From: Inflight calibration of the optical navigation camera for the extended mission phase of Hayabusa2

Sensitivity (DN/s)/(W/m2/µm/sr) at TCCD, T = -30 °C

 

Filters

ul

b

v

Na

w

x

P

Before TD1a

Sensitivity

439.1 ± 2.2

969 ± 7.9

1175.0 ± 10.0

546.9 ± 2.0

1515.0 ± 19.3

1499.8 ± 24.6

961.2 ± 28.8b

After TD1

Sensitivity

410.1 ± 11.6

899.1 ± 22.2

1092.8 ± 25.5

510.9 ± 12.2

1418.9 ± 35.1

1405.8 ± 40.7

898.9 ± 39.8

After TD2

Degradation trend

− 0.000252 day−1

Sensitivity at TD2

399.7 ± 10.8

879.6 ± 22.1

1071.2 ± 25.0

498.3 ± 11.9

1380.5 ± 34.0

1373.5 ± 37.4

882.6 ± 38.9

After capsule re-entry

Sensitivity

363.3 ± 9.0

810.2 ± 16.1

988.5 ± 10.3

469.5 ± 6.7

1279.4 ± 21.8

1276.7 ± 38.2

806.2 ± 30.1c

  1. aTatsumi et al. (2019). bValue based on lunar observations. cValue from observing the same star at different times