gptkbp:instance_of
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gptkb:satellite
|
gptkbp:collection
|
scientific data collection
real-time data acquisition
|
gptkbp:communication
|
high-speed data transmission
data relay
data relay capabilities
advanced communication system
|
gptkbp:controls
|
autonomous control system
|
gptkbp:country
|
gptkb:China
|
gptkbp:data_usage
|
high data transmission rate
|
gptkbp:debut_year
|
gptkb:2016
|
gptkbp:decommissioned
|
gptkb:battle
|
gptkbp:design
|
3 years
2016-002 A
|
gptkbp:elevation
|
approximately 36,000 km
|
gptkbp:first_flight
|
testing new technologies
|
gptkbp:home_ground
|
gptkb:Beijing
|
https://www.w3.org/2000/01/rdf-schema#label
|
Shijian-17
|
gptkbp:is_capable_of
|
advanced capabilities
|
gptkbp:is_tested_for
|
new satellite technologies
|
gptkbp:launch_date
|
2016-01-09
|
gptkbp:launch_site
|
gptkb:Taiyuan_Satellite_Launch_Center
gptkb:China_National_Space_Administration
|
gptkbp:launch_vehicle
|
gptkb:Long_March_4_B
1,000 kg
|
gptkbp:launched
|
January 2016
|
gptkbp:manufacturer
|
gptkb:China_Academy_of_Space_Technology
|
gptkbp:mass
|
approximately 1,000 kg
|
gptkbp:mission
|
gptkb:satellite
successful launch
evaluate new technologies
test new technologies
demonstration mission
DFH-4
technology demonstration satellite
demonstration of satellite technologies
deployed in orbit
|
gptkbp:mission_duration
|
5 years
|
gptkbp:molt
|
2016-002 A
|
gptkbp:operational_status
|
operational
|
gptkbp:operator
|
gptkb:China
|
gptkbp:orbital_inclination
|
0 degrees
|
gptkbp:orbital_period
|
24 hours
|
gptkbp:power_output
|
solar panels
|
gptkbp:propulsion
|
modular design
experimental spacecraft
standard configuration
operational in orbit
|
gptkbp:purpose
|
technology demonstration
|
gptkbp:reliability
|
high
|
gptkbp:seating_capacity
|
1,000 kg
experimental payloads
varied payloads
|
gptkbp:status
|
active
|
gptkbp:successor
|
gptkb:Shijian-18
|
gptkbp:track
|
ground stations
tracked by ground stations
|
gptkbp:type
|
experimental satellite
|
gptkbp:bfsParent
|
gptkb:Shijian_Satellites
|
gptkbp:bfsLayer
|
5
|