|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
geosynchronous satellite launch
|
|
gptkbp:associated_missions
|
gptkb:INSAT_series
|
|
gptkbp:challenges
|
gptkb:overcome
|
|
gptkbp:collaboration
|
limited
|
|
gptkbp:collaborative_projects
|
with universities
|
|
gptkbp:contribution
|
gptkb:significant
|
|
gptkbp:debut
|
multiple successful missions
|
|
gptkbp:design
|
approximately 15 years
indigenous
|
|
gptkbp:development
|
1990s
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:educational_value
|
inspiring future engineers
|
|
gptkbp:engine
|
gptkb:ISRO_Propulsion_Complex
|
|
gptkbp:engine_type
|
cryogenic engine
|
|
gptkbp:environmental_concerns
|
addressed
|
|
gptkbp:equipment
|
advanced materials
|
|
gptkbp:first_flight
|
gptkb:2010
successful
|
|
gptkbp:fuel_type
|
cryogenic liquid
|
|
gptkbp:future_prospects
|
high
|
|
gptkbp:global_standing
|
improved
|
|
gptkbp:height
|
12.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GSLV Cryogenic Upper Stage (GCU)
|
|
gptkbp:impact_on_space_industry
|
gptkb:significant
|
|
gptkbp:involved_technology
|
liquid propulsion
|
|
gptkbp:key_feature
|
cryogenic technology
|
|
gptkbp:launch_date
|
periodic
|
|
gptkbp:launch_site
|
gptkb:Satish_Dhawan_Space_Centre
|
|
gptkbp:launch_vehicle
|
gptkb:GSLV
|
|
gptkbp:manufacturer
|
gptkb:ISRO
|
|
gptkbp:mission
|
satellite deployment
|
|
gptkbp:notable_launches
|
gptkb:GSAT_series
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:operational_since
|
gptkb:2010
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:operational_use
|
upper stage propulsion
|
|
gptkbp:part_of
|
gptkb:Indian_space_program
|
|
gptkbp:payload_capacity
|
up to 2,500 kg to GTO
|
|
gptkbp:project
|
gptkb:GSLV_Mk_III
|
|
gptkbp:propulsion
|
liquid oxygen and liquid hydrogen
200 k N
|
|
gptkbp:public_perception
|
positive
|
|
gptkbp:reliability
|
proven
|
|
gptkbp:research_and_development
|
ongoing
|
|
gptkbp:safety_measures
|
implemented
|
|
gptkbp:significance
|
enhanced payload capacity
|
|
gptkbp:specific_impulse
|
450 seconds
|
|
gptkbp:specification
|
documented
|
|
gptkbp:strategic_importance
|
gptkb:national_security
|
|
gptkbp:success_rate
|
high
|
|
gptkbp:technology
|
cryogenic propulsion
|
|
gptkbp:upgrades
|
planned
|
|
gptkbp:used_in
|
gptkb:GSLV_rocket
|
|
gptkbp:weight
|
around 4 tons
|
|
gptkbp:bfsParent
|
gptkb:GSLV
|
|
gptkbp:bfsLayer
|
5
|