|
gptkbp:instance_of
|
gptkb:satellite
|
|
gptkbp:availability
|
redundant systems
|
|
gptkbp:communication
|
telecommunications services
C-band
Ku-band
Ka-band
|
|
gptkbp:connects
|
702 bus
|
|
gptkbp:cooling_system
|
active thermal control system
|
|
gptkbp:data_bus_width
|
three-axis stabilized
|
|
gptkbp:data_usage
|
up to 1 Gbps
|
|
gptkbp:debut_year
|
multiple successful launches
|
|
gptkbp:design
|
15 years
|
|
gptkbp:developer
|
gptkb:Boeing_702_series
|
|
gptkbp:end_of_life
|
decommissioned after 15 years
|
|
gptkbp:first_flight
|
gptkb:2014
|
|
gptkbp:frequency
|
multiple frequency bands
|
|
gptkbp:healthcare
|
advanced telemetry systems
|
|
gptkbp:home_ground
|
Boeing ground control systems
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Boeing 702 MP
|
|
gptkbp:launch_date
|
2014-01-23
|
|
gptkbp:launch_site
|
gptkb:United_Launch_Alliance
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launch_vehicle
|
gptkb:Atlas_V
approximately 6,000 kg
|
|
gptkbp:manufacturer
|
gptkb:aircraft
|
|
gptkbp:market
|
approximately $200 million
|
|
gptkbp:mass
|
approximately 6,000 kg
|
|
gptkbp:mission
|
gptkb:Boeing_702_bus
modular design
geostationary
commercial missions
high-gain antennas
part of satellite networks
|
|
gptkbp:notable_users
|
gptkb:Hispasat
gptkb:Telesat
gptkb:Eutelsat
gptkb:Intelsat
SESS. A.
|
|
gptkbp:orbital_inclination
|
0 degrees
|
|
gptkbp:powers
|
10 k W
|
|
gptkbp:propulsion
|
chemical propulsion
geostationary satellite
solar power system
|
|
gptkbp:purpose
|
communications
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:seating_capacity
|
up to 3,000 kg
up to 20 transponders
10 k W
|
|
gptkbp:service_area
|
global coverage
|
|
gptkbp:status
|
operational
|
|
gptkbp:sustainability
|
deployable solar arrays
|
|
gptkbp:track
|
high-precision tracking systems
|
|
gptkbp:transponders
|
broadband transponders
|
|
gptkbp:bfsParent
|
gptkb:Intelsat_29e
gptkb:Intelsat_35e
|
|
gptkbp:bfsLayer
|
4
|