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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:GSLV-F04
|
|
gptkbp:controls
|
Digital control system
|
|
gptkbp:country
|
gptkb:India
|
|
gptkbp:debut_year
|
gptkb:CEO
gptkb:GSLV-F04
|
|
gptkbp:developer
|
gptkb:CEO
|
|
gptkbp:engine
|
gptkb:4
|
|
gptkbp:engine_type
|
Liquid and cryogenic
|
|
gptkbp:events
|
Successful
|
|
gptkbp:first_flight
|
gptkb:CEO
2017-06-05
|
|
gptkbp:guidance_system
|
Inertial navigation system
|
|
gptkbp:height
|
49 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GSLV-F05
|
|
gptkbp:launch_date
|
2017-06-05
2017-06-05 T00:00:00 Z
|
|
gptkbp:launch_site
|
gptkb:Satish_Dhawan_Space_Centre
gptkb:ISRO
|
|
gptkbp:launch_vehicle
|
gptkb:GSLV-F05
gptkb:GSLV
gptkb:GSLV_Mk_II
Mk II
420 tonnes
Heavy lift
|
|
gptkbp:launched
|
gptkb:musical
gptkb:ISRO
gptkb:CEO
Automated
Second Launch Pad
|
|
gptkbp:manufacturer
|
gptkb:ISRO
|
|
gptkbp:mission
|
gptkb:ISRO_Telemetry,_Tracking_and_Command_Network
gptkb:battle
gptkb:satellite
Satellite launch
Geostationary transfer orbit
|
|
gptkbp:mission_duration
|
gptkb:CEO
|
|
gptkbp:number_of_stages
|
gptkb:3
gptkb:rocket
Liquid rocket engine
Cryogenic upper stage
|
|
gptkbp:operator
|
gptkb:ISRO
|
|
gptkbp:propulsion
|
5000 k N
|
|
gptkbp:released
|
Completed
|
|
gptkbp:restoration
|
gptkb:CEO
|
|
gptkbp:seating_capacity
|
gptkb:GSAT-19
Successful
4 m
2000 kg
2500 kg
|
|
gptkbp:succeeded_by
|
gptkb:theorem
|
|
gptkbp:tour
|
Sequential
|