THURAYA SATELLITE SPECIFICATIONS

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Customer

Thuraya Satellite
Telecommunications Co. Ltd.,
Abu Dhabi, United Arab Emirates

Product

GEO-mobile satellite
communications system
2 HS-GEM satellites
Primary gateway station
235,000 telephones

Launch

#1 #2

Date

Early 2000 Ground Spare

Vehicle

Sea Launch/
Ariane 5
TBD

Orbital Slot

44° E 28.5° E

Contract life

12 years 12 years

 

Space Segement

L-band
128 active elements
17-w SSPAs

C-band
2 active (2 spare)
feeder link
125-w TWTAs

 

Solar
 Beginning of life
 End of life
 Panels

13 kw
11 kw
2 wings of 4 panels each
w/dual-junction gallium
arsenide cells
Batteries 250 A-hr cells


Liquid apogee
motor

98 lbf (436N)

Stationkeeping
thrusters

  (bipropellant)

2 x 2 lbf (10N)
8 x 5 lbf (22N)

 

12.25 m (40 ft) x 16 m (52 ft) mesh transmit-receive reflector
128-element dipole L-band feed array
1.27 m round dual-polarized shaped reflector for C-band communications link

 

In orbit L, solar arrays: 34.5 m
(113 ft)
W, antennas: 17 m (55.7 ft)
Stowed H: 7.6 m (25 ft)
W: 3.75 m x 3.75 m
(12.3 ft)
Weights
 Launch
 In orbit
 (beginning of life)

5250 kg (11,576 lb)
3200 kg (7056 lb)