|
gptkbp:instanceOf
|
Launch vehicle
|
|
gptkbp:country
|
gptkb:India
|
|
gptkbp:developer
|
GSLV_program
|
|
gptkbp:engine
|
gptkb:Vikas_engine
|
|
gptkbp:firstFlight
|
2001
2003
2014
|
|
gptkbp:fuelType
|
Liquid propellant
|
|
gptkbp:height
|
49 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GSLV Mk II
|
|
gptkbp:launched
|
12
GSAT series satellites
|
|
gptkbp:launchSite
|
gptkb:Satish_Dhawan_Space_Centre
|
|
gptkbp:manufacturer
|
gptkb:ISRO
|
|
gptkbp:notableFeature
|
gptkb:GSAT-39
gptkb:GSAT-33
gptkb:GSAT-36
gptkb:GSAT-42
gptkb:GSAT-41
gptkb:GSAT-35
gptkb:GSAT-49
gptkb:GSAT-19
gptkb:GSAT-29
gptkb:GSAT-18
gptkb:GSAT-34
gptkb:GSAT-16
gptkb:GSAT-46
gptkb:GSAT-30
gptkb:GSAT-37
GSAT-31
GSAT-15
GSAT-12
GSAT-32
GSAT-38
GSAT-40
GSAT-43
GSAT-44
GSAT-45
GSAT-47
GSAT-48
GSAT-50
GSAT-5P
GSAT-6A
|
|
gptkbp:number_of_stages
|
3
|
|
gptkbp:orbitalInclination
|
Geostationary orbit
|
|
gptkbp:payloadCapacity
|
2,500 kg to Geostationary Transfer Orbit
|
|
gptkbp:performances
|
Solid, liquid, and cryogenic stages
|
|
gptkbp:productionCompany
|
1990
|
|
gptkbp:productionYears
|
2001-2014
|
|
gptkbp:propulsion
|
800 kN
|
|
gptkbp:provides
|
Inertial guidance system
|
|
gptkbp:replacedBy
|
gptkb:GSLV_Mk_III
|
|
gptkbp:setting
|
GSLV_Mk_II_configuration
|
|
gptkbp:skills
|
2
|
|
gptkbp:succeededBy
|
10
approximately 80%
|
|
gptkbp:usedFor
|
Satellite launches
|