|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:INSAT-4_CR
|
|
gptkbp:controls
|
gptkb:Inertial_Navigation_System
|
|
gptkbp:debut_year
|
gptkb:GSLV-F05
gptkb:GSLV-F06
|
|
gptkbp:developer
|
$100 million
|
|
gptkbp:engine_type
|
Liquid and Cryogenic
|
|
gptkbp:events
|
Successful
|
|
gptkbp:first_flight
|
gptkb:10
gptkb:2001
gptkb:2014
|
|
gptkbp:guidance_system
|
Onboard computer
|
|
gptkbp:healthcare
|
Real-time data transmission
|
|
gptkbp:height
|
49 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GSLV-F04
|
|
gptkbp:launch_date
|
2014-01-05
|
|
gptkbp:launch_site
|
gptkb:Satish_Dhawan_Space_Centre
gptkb:ISRO
|
|
gptkbp:launch_vehicle
|
gptkb:GSLV
2000 kg
|
|
gptkbp:launched
|
gptkb:Open
2 years
Second Launch Pad
|
|
gptkbp:manufacturer
|
gptkb:ISRO
|
|
gptkbp:mass
|
420 tons
|
|
gptkbp:mission
|
Satellite launch
Communication satellite deployment
Geostationary Transfer Orbit
|
|
gptkbp:mission_duration
|
15 years
|
|
gptkbp:number_of_stages
|
gptkb:3
gptkb:rocket
Liquid rocket engine
Cryogenic upper stage
|
|
gptkbp:restoration
|
Not applicable
|
|
gptkbp:seating_capacity
|
gptkb:GSAT-14
500 kg to Geosynchronous Transfer Orbit
|
|
gptkbp:setting
|
gptkb:GSLV_Mk_II
|
|
gptkbp:succeeded_by
|
gptkb:theorem
10%
|
|
gptkbp:track
|
Ground stations
|