Image
Imager for Magnetopause-to-Aurora Global Exploration
The Image mission will use three dimensional imaging techniques to study the
global response of the Earth's magnetosphere to variations in the magnetic
activity of the Sun. It will be the first satellite that will take pictures of
the magnetosphere as it changes shape.
The satellite is part of NASA's Midex program. It costs $40 million
http://image.gsfc.nasa.gov/
sat-index articles
Out
of service
|
late
2005?
|
Cause
|
Power
failure, then declared a failure after reboot in 2007
But in 2018, contact was rediscovered with telemetry on
|
Decay
|
|
Prime
contractor
|
Lockheed
Martin
|
Platform
|
LM100
|
Mass
at launch
|
494
kg
|
Mass
in orbit
|
|
Dimension
|
2.25
m diameter x 1.52 m height
|
Solar
array
|
|
Stabilization
|
spin-stabilized
(0.5 rpm)
|
DC
power
|
250
W
|
Design
lifetime
|
2
years
|
The IMAGE spacecraft has 3 antennas for S-band communication with the ground: a
medium-gain helix antenna and two low-gain omni-directional antennas.
Downlink rate: 2.28 Mbps (every 14.2 hours) plus a realtime transmission at 44
kbps.
Uplink rate: 2 kbps (once a week)
Communication via the Deep Space Network
Image carries six instruments: HENA (High Energy Neutral Atom; 10-500
keV) imager, MENA (Medium Energy Neutral Atom; 1-30 keV) imager, LENA (Low
Energy Neutral Atom; 10-500 eV) imager, FUV (Far Ultra-Violet) imager, EUV
(Extreme Untra-Violet) imager, and RPI (Radio Plasma Imager).
HENA, MENA, and LENA synthesize images from the arrival directions and
mass/energy of each neutral particle. (The energetic neutrals form an ephemeral
population when energetic ions charge-exchange with the thermal population.)
FUV carries three separate detectors: WIC (Wide Angle Camera) to image aurora
in a broad band and high spatial resolution (based on the UVI aboard
Polar),
SI (Spectroscopic Imager) to image aurora at selected wavelengths, and GEO
(GEOcorona) to image overall magnetospheric hydrogen atoms. EUV images the
population of He+ through the resonantly scattered solar radiation at 30.4 nm
wavelength. Finally, RPI consists of a pulsed transmitter (stepped 3 kHz to 3
MHz, 134 W peak) and a receiver, backed a radial dipole of 500 m length,
another orthogonal 500 m dipole, and an axial 20 m dipole, to get echoes from
boundary regions in the magnetosphere.