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Earth Observing-1 Launch Successful
Earth Observing - 1 (EO-1) was launched successfully on 21st Nov. at 1:24pm EST.
Earth Observing-1 Mission
The Earth Observing-1 (EO-1) Mission will fly in a 705 km circular,
sun-synchronous orbit at a 98.7 degree inclination. This orbit allows EO-1
to match within one minute, the Landsat 7 orbit and collect identical
images for later comparison on the ground. EO-1 has three advanced land
imaging instruments and seven revolutionary crosscutting spacecraft
technologies. The three advanced imaging instruments will lead to a new
generation of lighter weight, higher performance and lower cost
Landsat-type imaging instruments for the Earth Science Enterprise.
Additionally, the EO-1 Mission will flight validate a number of
crosscutting spacecraft subsystem technologies which if successful, will
enable future Earth and Space Science missions to be conducted using
smaller, lower weight and reduced power spacecraft buses.
Earth Observing-1 (EO-1) Instruments
The three primary instruments on the EO-1 spacecraft are the Advanced Land
Imager (ALI), the Hyperion and the Linear Etalon Imaging Spectrometer Array
(LEISA) Atmospheric Corrector (LAC). The EO-1 ALI consists of a 15f Wide
Field Telescope (WFT) and partially populated focal plane occupying 1/5th
of the field-of-view, giving a ground swath width of 37 km. Hyperion is a
grating imaging spectrometer having a 30 meter ground sample distance over
a 7.5 kilometer swath and providing 10nm (sampling interval) contiguous
bands of the solar reflected spectrum from 400-2500nm. LAC is an imaging
spectrometer covering the spectral range from 900 to 1600 nm which is well
suited to monitor the atmospheric water absorption lines for correction of
atmospheric effects in multispectral imagers such as ETM+ on Landsat. A
summary of instrument characteristics is given in Figure 1. Details of the
three instrument characteristics are provided in the following sections. A
comparison with Landsat 7 is included.
| Parameters |
Landsat 7 ETM+ |
EO-1 ALI |
EO-1 Hyperion |
EO-1 LAC |
| Spectral Range |
0.4-2.4µm |
0.4-2.4µm |
0.4-2.5µm |
0.9-1.6µm |
| Spatial Resolution |
30m |
30m |
30m |
250m |
| Panchromatic |
15m |
10m |
N/A |
N/A |
| Swath Width |
185km |
37km |
7.5km |
185km |
| Spectral Resolution |
variable |
variable |
10nm |
2-6nm |
| Spectral Coverage |
discrete |
discrete |
continuous |
continuous |
| Number of Bands |
7 |
10 |
220 |
256 |
Earth Observing-1 (EO-1) Technologies
Seven crosscutting
technologies which will reduce the cost, mass and complexity of
future Earth observing spacecraft will be demonstrated by EO-1 and
will allow more scientific payload to fly on future missions:
- X-Band Phased Array Antenna
- Carbon-Carbon Radiator
- Lightweight Flexible Solar Array
- Wideband Advanced Recorder Processor
- Pulsed Plasma Thruster
- Enhanced Formation Flying
- Fiber Optic Data Bus
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