|
gptkbp:instance_of
|
gptkb:Space_Launch_System
|
|
gptkbp:collaboration
|
gptkb:None
|
|
gptkbp:configuration
|
gptkb:GSLV_Mk_III
|
|
gptkbp:country
|
gptkb:India
|
|
gptkbp:debut
|
First flight in 2017
|
|
gptkbp:design
|
15 years
|
|
gptkbp:design_purpose
|
To launch heavier payloads
|
|
gptkbp:development
|
Approx. 10 years
|
|
gptkbp:development_cost
|
Approx. $150 million
|
|
gptkbp:engine_type
|
Liquid and solid propulsion
|
|
gptkbp:first_flight
|
gptkb:Yes
TBD
2017-06-05
|
|
gptkbp:height
|
43.4 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GSLV Mk III-D1
|
|
gptkbp:key_feature
|
Heavy payload capacity
|
|
gptkbp:launch_date
|
gptkb:Annual
2017-06-05
|
|
gptkbp:launch_event
|
Successful
|
|
gptkbp:launch_mass
|
640 tonnes
|
|
gptkbp:launch_platform
|
gptkb:ISRO
|
|
gptkbp:launch_price
|
Approx. $20 million
|
|
gptkbp:launch_site
|
gptkb:Satish_Dhawan_Space_Centre
|
|
gptkbp:launch_vehicle
|
gptkb:GSLV
Expendable launch vehicle
Heavy class
|
|
gptkbp:launch_window
|
gptkb:Open
|
|
gptkbp:launched
|
Second Launch Pad
|
|
gptkbp:manufacturer
|
gptkb:ISRO
|
|
gptkbp:mission
|
gptkb:ISRO_Telemetry,_Tracking_and_Command_Network
gptkb:Yes
|
|
gptkbp:mission_type
|
Satellite launch
|
|
gptkbp:notable_mission
|
gptkb:GSAT-19
|
|
gptkbp:number_of_engines
|
gptkb:5
|
|
gptkbp:number_of_stages
|
gptkb:3
C25
S200
L110
|
|
gptkbp:operational_status
|
Active
|
|
gptkbp:operational_use
|
Commercial and government missions
|
|
gptkbp:orbital_altitude
|
Geostationary Transfer Orbit
|
|
gptkbp:payload_capacity
|
4 meters
4000 kg to GTO
ISRO facilities
|
|
gptkbp:primary_function
|
Satellite deployment
|
|
gptkbp:propulsion
|
5000 k N
|
|
gptkbp:reliability
|
gptkb:High
|
|
gptkbp:success
|
gptkb:Yes
|
|
gptkbp:success_rate
|
100%
|
|
gptkbp:supports
|
ISRO's facilities
|
|
gptkbp:type
|
Heavy lift launch vehicle
|
|
gptkbp:upgrades
|
gptkb:Yes
|
|
gptkbp:used_for
|
Geostationary satellite launches
|
|
gptkbp:weight
|
640 tonnes
|
|
gptkbp:bfsParent
|
gptkb:GSLV_Mk_III
|
|
gptkbp:bfsLayer
|
5
|