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MISR - Multi-angle Imaging SpectroRadiometer
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MISR Instrument


Cut-Away Drawing of the MISR Instrument
The Multi-angle Imaging SpectroRadiometer (MISR) instrument will provide a unique opportunity for studying the ecology and climate of Earth through the acquisition of global multiangle imagery on the daylit side of Earth.

There are many requirements that must be taken into account when designing an instrument like MISR. This section describes some of them, i.e. rationale for why MISR is designed the way it is. For example, it tells why there are nine cameras and why they are set at particular angles.

The following paragraphs are by no means a full specification of the instrument. However, they represent some of the major items, and it is hoped that this will give the reader an indication of the types of unique factors considered when an instrument of this kind is conceived. The section begins with a summary of the engineering specifications of the instrument and, for completeness, of the Terra spacecraft on which MISR will be flown.

To read an article about building an on-orbit sensor such as MISR, click here.

Specifications of the MISR Instrument

Mission life: 6 years
MISR Optical Bench
Instrument mass: 148 kg
Instrument power: Approximately 117 W peak, 75 W average
Data rate: 3.3 Megabits/second average, 9.0 Megabits/second peak
Global coverage time: Every 9 days, with repeat coverage between 2 and 9 days depending on latitude
Crosstrack swath width: 360 km common overlap of all 9 cameras
Nine pushbroom cameras: Named An, Af, Aa, Bf, Ba, Cf, Ca, Df, and Da where fore, nadir, and aft viewing cameras have names ending with letters f, n, a respectively and four camera designs are named A, B, C, D with increasing viewing angle respectively
View angles: 0, 26.1, 45.6, 60.0, and 70.5 degrees
Spectral coverage: 4 bands (blue, green, red, and near-infrared)
Detectors: Charge Coupled Devices (CCDs), each camera with 4 independent line arrays (one per filter), 1504 active pixels per line
Radiometric accuracy: 3% at maximum signal
Detector (focal plane) temperature: -5 ±0.1 degrees C (cooled by thermo-electric cooler)
Temperature of main structure: +5 degrees C
Builder: Jet Propulsion Laboratory, Pasadena, California, U.S.A.