|
gptkbp:instance_of
|
gptkb:Space_Launch_System
|
|
gptkbp:collaboration
|
gptkb:None
gptkb:Yes
|
|
gptkbp:configuration
|
gptkb:GSLV_Mk_III-M1
gptkb:GSLV_Mk_III-M2
gptkb:GSLV_Mk_III-M3
|
|
gptkbp:country
|
gptkb:India
|
|
gptkbp:country_of_origin
|
gptkb:India
|
|
gptkbp:debut
|
gptkb:GSAT-19
Extensive
TBD
6 launches
|
|
gptkbp:design_purpose
|
Launch satellites into orbit
Heavy payload launch
|
|
gptkbp:developed_by
|
gptkb:ISRO
|
|
gptkbp:development
|
gptkb:ISRO
|
|
gptkbp:development_cost
|
approximately $1 billion
Approx. $200 million
|
|
gptkbp:diameter
|
4 m
|
|
gptkbp:elevation
|
640 tonnes
|
|
gptkbp:engine_configuration
|
SCE-200
|
|
gptkbp:engine_type
|
Liquid and solid
|
|
gptkbp:failure_count
|
gptkb:1
|
|
gptkbp:first_commercial_payload
|
gptkb:GSAT-19
|
|
gptkbp:first_flight
|
gptkb:2014
gptkb:GSLV_Mk_III-D1
gptkb:Yes
Successful
2014-12-18
December 18, 2014
2017-06-05
|
|
gptkbp:height
|
43.4 meters
43.4 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GSLV Mk III
|
|
gptkbp:is_significant_for
|
India's space program
|
|
gptkbp:launch_date
|
gptkb:Annual
gptkb:Regular
2023-10-05
2014-12-18
|
|
gptkbp:launch_event
|
Successful
|
|
gptkbp:launch_price
|
Approx. $30 million
|
|
gptkbp:launch_site
|
gptkb:Satish_Dhawan_Space_Centre
|
|
gptkbp:launch_vehicle
|
gptkb:High
gptkb:Space_Launch_System
gptkb:GSLV_family
2
Indigenous
Heavy-lift launch vehicle
S200
Geosynchronous launch vehicle
|
|
gptkbp:launch_window
|
Flexible
|
|
gptkbp:launched
|
multiple
|
|
gptkbp:liquid_core_stage
|
gptkb:1
L110
|
|
gptkbp:liquid_fuel
|
LH2 and LOX
|
|
gptkbp:liquid_upper_stage
|
C25
|
|
gptkbp:manufacturer
|
gptkb:ISRO
|
|
gptkbp:mission
|
gptkb:ISRO_Telemetry,_Tracking_and_Command_Network
Planned
|
|
gptkbp:notable_achievement
|
First Indian rocket to carry a payload of 4 tons to GTO.
|
|
gptkbp:notable_mission
|
gptkb:Chandrayaan-2
gptkb:GSAT-19
gptkb:GSAT-29
gptkb:GSAT-30
gptkb:Gaganyaan
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_since
|
gptkb:2014
|
|
gptkbp:operational_status
|
Active
active
|
|
gptkbp:orbital_insertion_capability
|
gptkb:Yes
|
|
gptkbp:payload_capacity
|
gptkb:GSAT-19
5 meters
4000 kg
5.0 meters
4000 kg to GTO
4,000 kg to GTO
|
|
gptkbp:propulsion
|
5000 k N
|
|
gptkbp:reliability
|
gptkb:High
|
|
gptkbp:replaced_by
|
gptkb:GSLV_Mk_III-M1
|
|
gptkbp:significance
|
India's heavy-lift capability
|
|
gptkbp:solid_booster
|
2
|
|
gptkbp:success
|
gptkb:5
|
|
gptkbp:success_count
|
gptkb:5
|
|
gptkbp:success_rate
|
gptkb:High
100%
high
0%
|
|
gptkbp:successor
|
gptkb:GSLV_Mk_II
|
|
gptkbp:upgrades
|
gptkb:Yes
|
|
gptkbp:used_for
|
Geostationary satellite launches
|
|
gptkbp:bfsParent
|
gptkb:Chandrayaan-2
gptkb:Indian_Space_Research_Organisation
gptkb:Vikram
|
|
gptkbp:bfsLayer
|
4
|