Inmarsat-5 F3

Inmarsat

Spacecraft nº:

Inmarsat spacecraft nº: 16


Launch data:

Designation 40882 / 15042A
Launch date 28 Aug 2015 - 11:44 UT
Launch site Baik, LC-200/39
Launch vehicle  Proton-M /Briz-M
Mission 
Geostationary orbit:
Perigee / Apogee 31521 x 41016 km
Eccentricity 
Inclination 0.2 °
Period 1436.2 min
Inmarsat 5


Spacecraft data:

Prime manufacturer Boeing Satellite Systems
Platform BSS-702HP
Operator Inmarsat
Mass at launch  5900 kg; BOL: 3750 kg
Dry Mass  kg
Basic shape  box
Dimension (stowed) H= 6.98 m, W= 3.59 m, L= 3.27m
Dimension (in orbit) H= 6.98 m, W antennas= 8.08 m, L solar arrays= 33.80 m
>Equipment and Antennas
Antenna Ka 89 user beams generated by 2 transmit and 4 receive apertures
Repeater Ka Bent-pipe repeater, Ka-band: 60:48 TWTAs
T&C RF Ka and C-band
High Capacity Six steerable spot beams fed by 12 130W TWTAs
Solar array 2 deployable solar arrays
Stabilization  
Propulsion:
Liquid apogee engine 445 N
Stationkeeping Thrusters Xenon ion propulsion
Control Thrusters 4 x 22N (Axial), 4 x 10N (radial)
Power
Solar Panels 13.8 kW, end of life
Construction Two wings each with five panels of gallium arsenide solar cells
Batteries Dual Li-Ion batteries
Design lifetime  15 yrs



Inmarsat-5 F3



Description:

External links:


Ref.: #7(JR715), #110, #228, #www.boeing.com - update: 28.01.16 Home