TDRS 7
Also called TDRS G
Begin
|
End
|
Position
|
L:
13 Jul 1995
|
May
1996
|
150°W
(testing)
|
Jun
1996
|
Dec
2003
|
171°W
(spare)
|
Jan
2004
|
Jun
2009
|
150.5°W
+/- 0.3°
|
Jul
2009
|
|
85°E
|
The IUS consists of two Solid Rocket Motors (SRM's) which inject the TDRS/IUS
into geostationary orbit. The IUS SRM 1 first place the TDRS/IUS into a
transfer orbit with an apogee near geosynchronous altitude (burn at 20:55 UT).
At the first apogee the IUS SRM 2 fired to place the TDRS/IUS in geostationary
orbit (14 Jul at 02:30 UT). The TDRS/IUS was then maneuvered to the appropriate
orientation and TDRS 7 separated from the IUS.
sat-index articles
Specifications
S-band
Ku-band
Has no C-band capacity.