gptkbp:instance_of
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gptkb:Space_Launch_System
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gptkbp:control_system
|
Inertial navigation system
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gptkbp:country
|
gptkb:India
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gptkbp:developed_by
|
gptkb:ISRO
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gptkbp:development
|
gptkb:1990
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gptkbp:diameter
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2.8 m
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gptkbp:engine_type
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liquid fuel
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gptkbp:first_flight
|
gptkb:2001
gptkb:2003
gptkb:2014
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gptkbp:flight_style
|
gptkb:14
|
gptkbp:guidance_system
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gptkb:GPS
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gptkbp:height
|
49 m
49 meters
|
https://www.w3.org/2000/01/rdf-schema#label
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GSLV Mk II
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gptkbp:launch_mass
|
420 tons
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gptkbp:launch_site
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gptkb:Satish_Dhawan_Space_Centre
|
gptkbp:launched
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gptkb:INSAT_series
gptkb:GSAT_series
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gptkbp:liquid_fuel
|
UDMH and N2 O4
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gptkbp:manufacturer
|
gptkb:ISRO
|
gptkbp:notable_launches
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gptkb:GSAT-6_A
gptkb:GSAT-39
gptkb:GSAT-33
gptkb:GSAT-36
gptkb:GSAT-42
gptkb:GSAT-41
gptkb:GSAT-19
gptkb:GSAT-29
gptkb:GSAT-34
gptkb:GSAT-31
gptkb:GSAT-32
gptkb:GSAT-44
gptkb:GSAT-47
gptkb:GSAT-48
gptkb:GSAT-50
gptkb:GSAT-16
gptkb:GSAT-46
gptkb:GSAT-30
gptkb:GSAT-37
gptkb:INSAT-3_A
gptkb:INSAT-3_B
gptkb:INSAT-3_C
gptkb:INSAT-3_DR
gptkb:GSAT-15
GSAT-38
GSAT-40
GSAT-43
GSAT-45
GSAT-35
GSAT-49
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gptkbp:number_of_stages
|
gptkb:3
gptkb:Team_Rocket
Cryogenic upper stage
Liquid core stage
|
gptkbp:orbital_inclination
|
Geostationary orbit
|
gptkbp:payload_capacity
|
2,500 kg
|
gptkbp:replaced_by
|
gptkb:GSLV_Mk_III
|
gptkbp:solid_booster
|
2
|
gptkbp:success
|
gptkb:10
|
gptkbp:success_rate
|
75%
25%
|
gptkbp:used_for
|
geostationary satellite launches
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gptkbp:bfsParent
|
gptkb:Chandrayaan-2
gptkb:Vikram
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gptkbp:bfsLayer
|
4
|