2000-01
AUTHORSW.C. Gibson, J.L. Burch, J.R. Scherrer, M.B. Tapley, R.L. Killough, F.A. Volpe, W.D. Davis, D.C. Vaccarello, G. Grismore, D. Sakkas, S.J. Housten
ABSTRACTThe Imager for Magnetopause-to-Aurora Global Exploration (IMAGE) mission will be the first of the new Medium-class Explorer (MIDEX) missions to fly. IMAGE will utilize a combination of ultraviolet and neutral atom imaging instruments plus an RF sounder to map and image the temporal and spatial features of the magnetosphere. The eight science sensors are mounted to a single deckplate. The deckplate is enveloped in an eight-sided spacecraft bus, 225 cm across the flats, developed by Lockheed Martin Missiles and Space Corporation. Constructed of laminated aluminum honeycomb panels, covered extensively by Gallium Arsenide solar cells, the spacecraft structure is designed to withstand the launch loads of a Delta 7326-9.5 ELV. Attitude control is via a single magnetic torque rod and passive nutation damper with aspect information provided by a star camera, sun sensor, and three-axis magnetometer. A single S-band transponder provides telemetry and command functionality. Interfaces between the self-contained payload and the spacecraft are limited to MIL-STD-1553 and power. This paper lists the requirements that drove the design of the IMAGE Observatory and the implementation that met the requirements. More... »
PAGES15-50
http://scigraph.springernature.com/pub.10.1023/a:1005203207186
DOIhttp://dx.doi.org/10.1023/a:1005203207186
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