2015A&A...574A.123M


Query : 2015A&A...574A.123M

2015A&A...574A.123M - Astronomy and Astrophysics, volume 574A123-123 (2015/2-1)

Pre-hibernation performances of the OSIRIS cameras onboard the Rosetta spacecraft.

MAGRIN S., LA FORGIA F., DA DEPPO V., LAZZARIN M., BERTINI I., FERRI F., PAJOLA M., BARBIERI M., NALETTO G., BARBIERI C., TUBIANA C., KUEPPERS M., FORNASIER S., JORDA L. and SIERKS H.

Abstract (from CDS):

The ESA cometary mission Rosetta was launched in 2004. In the past years and until the spacecraft hibernation in June 2011, the two cameras of the OSIRIS imaging system (Narrow Angle and Wide Angle Camera, NAC and WAC) observed many different sources. On 20 January 2014 the spacecraft successfully exited hibernation to start observing the primary scientific target of the mission, comet 67P/Churyumov-Gerasimenko. A study of the past performances of the cameras is now mandatory to be able to determine whether the system has been stable through the time and to derive, if necessary, additional analysis methods for the future precise calibration of the cometary data. The instrumental responses and filter passbands were used to estimate the efficiency of the system. A comparison with acquired images of specific calibration stars was made, and a refined photometric calibration was computed, both for the absolute flux and for the reflectivity of small bodies of the solar system. We found a stability of the instrumental performances within ±1.5% from 2007 to 2010, with no evidence of an aging effect on the optics or detectors. The efficiency of the instrumentation is found to be as expected in the visible range, but lower than expected in the UV and IR range. A photometric calibration implementation was discussed for the two cameras. The calibration derived from pre-hibernation phases of the mission will be checked as soon as possible after the awakening of OSIRIS and will be continuously monitored until the end of the mission in December 2015. A list of additional calibration sources has been determined that are to be observed during the forthcoming phases of the mission to ensure a better coverage across the wavelength range of the cameras and to study the possible dust contamination of the optics.

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Journal keyword(s): instrumentation: detectors - space vehicles: instruments - techniques: photometric

Simbad objects: 31

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Number of rows : 31
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 HD 36591 V* 05 32 41.3510096736 -01 35 30.595447356 4.240 5.15 5.34     B1IV 255 0
2 * eta Hya bC* 08 43 13.4757536071 +03 23 55.182801587 3.380 4.100 4.300 4.37 4.56 B3V 418 1
3 * tet Vir ** 13 09 56.9889385680 -05 32 20.414634792   4.385 4.397     A1IVs 277 0
4 * d Her * 17 01 36.3612969768 +33 34 05.766475152   5.288 5.267     A3IV 113 0
5 * 38 Oph ** 17 17 39.53024 -26 37 44.4788           B9.5V 23 0
6 * iot Her bC* 17 39 27.8868980278 +46 00 22.792978043 2.940 3.630 3.800     B3IV 470 1
7 HD 162161 * 17 48 47.8706558544 +19 15 18.048711816   6.147 6.125     A1V 41 0
8 * 9 Sgr Y*O 18 03 52.4450051016 -24 21 38.632254012 5.08 5.97 5.97 5.72 5.70 O4V((f))z 563 0
9 * 102 Her * 18 08 45.4919267342 +20 48 52.404584093 3.38 4.177 4.347     B2IV 194 0
10 * alf Lyr dS* 18 36 56.33635 +38 47 01.2802 0.03 0.03 0.03 0.07 0.10 A0V 2787 1
11 HD 176318 SB* 18 58 01.8981886272 +38 15 58.279524552   5.787 5.883     B7IV 97 0
12 * iot Lyr Be* 19 07 18.1323268968 +36 06 00.572464476 4.66 5.137 5.253     B6IV 120 0
13 * 20 Aql V* 19 12 40.7117853648 -07 56 22.263784872 5.03 5.47 5.34     B2/3II 240 0
14 HD 181828 * 19 20 33.0559684632 +35 11 09.456123912 5.81 6.188 6.290     B9V 58 0
15 * 9 Vul V* 19 34 34.8970506960 +19 46 24.242282112 4.48 4.91 5.00 5.01 5.10 B8IIIn 99 0
16 HD 185330 V* 19 36 56.6493724800 +38 23 01.768931556 5.72 6.368 6.500     B5II-III 73 0
17 * 16 Cyg A ** 19 41 48.9534996168 +50 31 30.219536784 6.79 6.59 5.95 5.50 5.17 G1.5Vb 814 0
18 * 16 Cyg ** 19 41 49.09 +50 31 31.6           ~ 166 0
19 * 16 Cyg B PM* 19 41 51.9726777456 +50 31 03.089030916 7.07 6.86 6.20 5.76 5.42 G3V 949 1
20 V* V380 Cyg SB* 19 50 37.3267754400 +40 35 59.135141652 4.86 5.613 5.680     B1.1III+B2.5/3V: 305 0
21 HD 188252 Pu* 19 52 07.1662436976 +47 55 54.461806320 4.87 5.722 5.897     B2III 84 0
22 * 9 Sge s*b 19 52 21.7649260368 +18 40 18.751320984 5.32 6.24 6.23     O7.5Iabf 308 1
23 * 11 Sge * 19 57 45.4454745624 +16 47 20.978081988 5.31 5.480 5.534     B9III 75 0
24 HD 189689 Be* 20 00 07.0577245152 +32 47 22.837948944   7.230 7.277     B9 34 0
25 HD 191243 s*b 20 07 41.4408550416 +34 25 22.464338340 6.09 6.248 6.141     B5II 93 0
26 * nu. Cap * 20 20 39.8157949497 -12 45 32.690284207 4.61 4.72 4.76 4.75 4.81 B9IV 279 0
27 HD 196775 * 20 39 04.9680556008 +15 50 17.511192132 5.110 5.820 5.980     B3V 66 0
28 HD 199478 s*b 20 55 49.8039729168 +47 25 03.564093468 5.79 6.12 5.64 5.16 4.78 B7Ia 231 0
29 HD 199579 Y*O 20 56 34.7779063080 +44 55 29.000891928 5.16 6.01 5.96     O6.5V((f))z 375 0
30 * 60 Cyg Be* 21 01 10.9277453472 +46 09 20.795190696 4.23 5.226 5.432     B1Ve 217 0
31 * 69 Cyg s*b 21 25 47.0250895464 +36 40 02.584183260 4.89 5.86 5.94     B0.2Iab 207 0

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