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The Coriolis satellite
will demonstrate the ability to measure wind speed and direction
on the world's oceans. In addition, on-board instruments will
track coronal mass ejections from the Sun as they propagate
through the interplanetary medium, providing advance warning of
geomagnetic disturbances. The instruments that will accomplish
these tasks are named WindSat and SMEI.
The Coriolis spacecraft
is a three-axis stabilized, nadir-pointing satellite that will be
inserted into a 830 km sun synchronous polar orbit at 98.7°
inclination. It is approximately 21 x 8 x 7 ft in size and has a
launch mass of about 817 kg (1800 lbm). An on-board hydrazine
propulsion system will be used to circularize the initial orbit
and provide orbit maintenance as the mission progresses. Coriolis
is expected to operate for a minimum of three years.
The WindSat payload
will demonstrate the capability of a polarimetric microwave
radiometer to measure the ocean surface wind vector on a global
scale. This will be the first such instrument to provide wind
direction as well as speed, and will allow a 3X increase in
performance over current systems. The multi-frequency radiometer
will operate in the 6.8, 10.7, 18.7, 23.8, and 37 GHz ranges. The
US Navy will use a real time S-band tactical downlink to
distribute radiometer data to deployed fleet units. This
technology demonstration is an important pathfinder for the
National Polar-orbiting Operational Environmental Satellite System
(NPOESS).
The Solar Mass
Ejection Imager (SMEI) payload will use an all-sky camera assembly
to monitor and track coronal mass ejections. Algorithms will be
used to convert this data into a 1-3 day warning of significant
geomagnetic disturbances on Earth. The three SMEI cameras provide
a 3° x 180° field of view with a 1° resolution.
Coriolis is a DoD Test
Program mission to fly Naval Research Laboratory (NRL) and Air
Force Research Laboratory (AFRL) payloads. Spectrum Astro’s
contract was competitively awarded in March 1999 through NASA
Goddard’s Rapid Spacecraft Development Office.

| Coriolis
|
|
SPACECRAFT
|
| Int'l Designation |
2003 001A
|
Launched
|
| Owner / Sponsor |
Naval
Research Laboratory (NRL) / Air Force Research Laboratory (AFRL)
|
| Mission |
Science
|
| Satellite Bus |
Spectrum
Astro
|
|
| Launch Mass |
816
kg (1800 lbm)
|
| Mission Orbit |
SSO /
830 km (448 nmi)
|
98.7°
|
| Design Life |
3
years
|
| Power (EOL) |
|
|
LAUNCH
|
| Launch Vehicle
Model |
Titan
2 |
| Launch Date / Time |
6 January
2003
|
14:19
|
|
FINANCIAL
|
| Satellite cost |
US$224
million
|
| Web Links |
Coriolis
Website
|
|