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181.
The Dawn Framing Camera 总被引:1,自引:0,他引:1
H. Sierks H. U. Keller R. Jaumann H. Michalik T. Behnke F. Bubenhagen I. B��ttner U. Carsenty U. Christensen R. Enge B. Fiethe P. Guti��rrez Marqu��s H. Hartwig H. Kr��ger W. K��hne T. Maue S. Mottola A. Nathues K.-U. Reiche M. L. Richards T. Roatsch S. E. Schr?der I. Szemerey M. Tschentscher 《Space Science Reviews》2011,163(1-4):263-327
The Framing Camera (FC) is the German contribution to the Dawn mission. The camera will map 4 Vesta and 1 Ceres through a clear filter and 7 band-pass filters covering the wavelengths from the visible to the near-IR. The camera will allow the determination of the physical parameters of the asteroids, the reconstruction of their global shape as well as local topography and surface geomorphology, and provide information on composition via surface reflectance characteristics. The camera will also serve for orbit navigation. The resolution of the Framing Camera will be up to 12 m per pixel in low altitude mapping orbit at Vesta (62 m per pixel at Ceres), at an angular resolution of 93.7 ??rad?px?1. The instrument uses a reclosable front door to protect the optical system and a filter-wheel mechanism to select the band-pass for observation. The detector data is read out and processed by a data processing unit. A power converter unit supplies all required power rails for operation and thermal maintenance. For redundancy reasons, two identical cameras were provided, both located side by side on the +Z-deck of the spacecraft. Each camera has a mass of 5.5 kg. 相似文献
182.
A. N. Parmar G. Hasinger M. Arnaud X. Barcons D. Barret H. Bhringer A. Blanchard M. Cappi A. Comastri T. Courvoisier A. C. Fabian F. Fiore I. Georgantopoulos P. Grandi R. Griffiths A. Hornstrup N. Kawai K. Koyama K. Makishima G. Malaguti K. O. Mason C. Motch M. Mendez T. Ohashi F. Paerels L. Piro T. Ponman J. Schmitt S. Sciortino G. Trinchieri M. van der Klis M. Ward 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2004,34(12):2623
Europe is one of the major partners building the International Space Station (ISS) and European industry, together with ESA, is responsible for many station components including the Columbus Orbital Facility, the Automated Transport Vehicle, two connecting modules and the European Robotic Arm. Together with this impressive list of contributions there is a strong desire within the ESA Member States to benefit from this investment by utilizing the unique capabilities of the ISS to perform world-class science. XEUS is one of the astronomical applications being studied by ESA to utilize the capabilities of the ISS. XEUS will be a long-term X-ray observatory with an initial mirror area of 6 m2 at 1 keV that will be expanded to 30 m2 following a visit to the ISS. The 1 keV spatial resolution is expected to be 2–5″ half-energy-width. XEUS will consist of separate detector and mirror spacecraft (MSC) aligned by active control to provide a focal length of 50 m. A new detector spacecraft, complete with the next generation of instruments, will also be added after visiting the ISS. The limiting 0.1–2.5 keV sensitivity will then be 4 × 10−18 erg cm−2 s−1, around 200 times better than XMM-Newton, allowing XEUS to study the properties of the hot baryons and dark matter at high redshift. 相似文献
183.
Abstract This paper investigates the impact of geometrical and nongeometrical features on the use of the lexical concepts NEAR and FAR in English and Finnish. Participants' acceptability ratings for these concepts demonstrate that a bar in between a Figure and a Ground acts as a scale-setting object but not as a distance enhancing barrier, shows that the influence of the geometrical feature Figure–Ground distance exceeds the influence of several nongeometrical features, but most of all reveals that language specific lexical properties associated with NEAR and FAR predict language dependent effects for functional relatedness in interaction with Figure–Ground distance and bar presence. 相似文献
184.
We investigate links between the observational environment as experienced by the Hipparcos satellite and the performance of
the spacecraft and payload instrumentation, with particular emphasis on finding out whether some of these effects may have
been inadequately represented in instrument calibrations and could thus have affected the scientific results of the mission.
Scan-coverage and radiation effects are primarily random effects with only some long-term systematics. However, long- (days
to weeks) and short-term (hours) temperature variations reflected in the performance of some of the spacecraft instrumentation.
It is shown that only a small sign of some long-term thermal variations could be detected in the payload instrumentation.
These findings further limit the scope left for the occurrence of large-scale correlated errors in the Hipparcos astrometric
data. On the other hand, a number of great circles were identified which showed a highly significant drift of the basic angle,
which had not been detected in the preparation of the published data. The data from these circles may have, in some cases,
led to, very localised, slightly anomalous results, in particular where stars are accidentally affected by two or more of
such circles.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献