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The 3192 kg (7031 lbm) satellite
was built by Boeing Satellite Systems, using a BSS 601 satellite
bus. The satellite carries S-, Ku- and Ka-band transponders. Each
TDRS satellite can receive data rates at 300 megabits/second
(Mbps) using Ku- and Ka-band, and 6 Mbps at S band. Each
spacecraft carries the additional capability for Ka-band receive
rates of up to 800 Mbps. Transmit data rates are 25 Mbps for Ku-
and Ka-band, and 300 kilobits/second (Kbps) for S-band. In
addition, the S-band phased array antenna can receive signals from
five spacecraft at once, while transmitting to one. The TDRS
satellites are unique in their ability to follow the motion of
fast moving spacecraft, providing nearly continuous communication
with controllers and researchers on Earth. In addition to the
International Space Station (ISS) and Space Shuttle, other
programs using the TDRS constellation include the Hubble Space
Telescope, STARlink, the Tropical Rainfall Measuring Mission (TRMM),
Landsat, and Earth Observing System (EOS). TDRS also provides
expendable-launch-vehicle tracking services to launch service
providers.
TDRS
10 (J)
Tracking
and Data
Relay
Satellite
|
|
SPACECRAFT
|
| Int'l Designation |
2002 055A
|
Launched
|
| Owner / Sponsor |
NASA
|
| Mission |
Telecommunication
|
| Constellation/Block |
TDRS
II
|
| Manufacturer |
Boeing
Satellite Systems
|
HS 601
|
| Launch Mass |
3192
kg (7031 lbm)
|
| Dimensions, stowed |
3.4
x 3.4 x 8.4 m (11 ft 8 in x 11 ft 8 in x 27 ft 8 in)
|
| Mission Orbit |
GSO
|
|
| Design Life |
11
years
|
| Power (EOL) |
2.300
kW
|
|
LAUNCH
|
| Launch Vehicle
Model |
Atlas
2A |
| Date / Time (UTC) |
5
December 2002
|
02:42
|
|
FINANCIAL
|
| Satellite cost |
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| Web Links |
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