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gptkbp:instance_of
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gptkb:Space_Launch_System
gptkb:Team_Rocket
|
|
gptkbp:challenges
|
developing cryogenic technology
|
|
gptkbp:collaboration
|
gptkb:various_countries
various space agencies
|
|
gptkbp:collaborative_projects
|
with foreign space agencies
|
|
gptkbp:contribution
|
global satellite communications
|
|
gptkbp:control_system
|
gptkb:navigation_system
digital flight control system
|
|
gptkbp:country
|
gptkb:India
|
|
gptkbp:country_of_origin
|
gptkb:India
|
|
gptkbp:debut
|
gptkb:2003
gptkb:2014
over 15 successful launches
|
|
gptkbp:design_features
|
indigenous cryogenic upper stage
|
|
gptkbp:design_philosophy
|
reliability and cost-effectiveness
|
|
gptkbp:development
|
gptkb:1990
1990s
|
|
gptkbp:development_cost
|
approximately $1 billion
|
|
gptkbp:engine
|
gptkb:Vikram_Sarabhai_Space_Centre
|
|
gptkbp:engine_type
|
liquid and solid
liquid and solid propulsion
|
|
gptkbp:first_cryogenic_flight
|
gptkb:2014
|
|
gptkbp:first_flight
|
gptkb:2001
gptkb:2003
|
|
gptkbp:fuel_type
|
UDMH and N2 O4
|
|
gptkbp:future_goals
|
enhanced payload capacity
|
|
gptkbp:future_plans
|
upgraded versions
upgraded versions in development
|
|
gptkbp:guidance_system
|
gptkb:navigation_system
|
|
gptkbp:has_programs
|
gptkb:satellite
|
|
gptkbp:has_weakness
|
GSLV D1, GSLV D5
|
|
gptkbp:height
|
49 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GSLV rocket
|
|
gptkbp:impact
|
significant contributions to space science
|
|
gptkbp:influenced_by
|
global space trends
|
|
gptkbp:international_recognition
|
significant player in space launches
|
|
gptkbp:involved_technology
|
to other nations
|
|
gptkbp:key_concept
|
cryogenic propulsion
|
|
gptkbp:latest_version
|
gptkb:GSLV_Mk_III
|
|
gptkbp:launch_date
|
August 2021
April 18, 2001
2-3 times a year
2-3 times per year
|
|
gptkbp:launch_event
|
gptkb:GSAT-15
multiple successful missions
|
|
gptkbp:launch_frequency_trend
|
increasing over the years
|
|
gptkbp:launch_platform
|
gptkb:ISRO_Telemetry,_Tracking_and_Command_Network
|
|
gptkbp:launch_price
|
approximately $20 million
|
|
gptkbp:launch_site
|
gptkb:Satish_Dhawan_Space_Centre
|
|
gptkbp:launch_vehicle
|
gptkb:GSLV_family
SLC-40
modular
expendable launch vehicle
medium-lift
from GSLV Mk I to Mk III
three-stage
|
|
gptkbp:launch_window
|
varies by mission
specific time frame
|
|
gptkbp:manufacturer
|
gptkb:ISRO
|
|
gptkbp:marketed_as
|
for international satellite launches
|
|
gptkbp:media_coverage
|
extensive during launches
|
|
gptkbp:mission
|
gptkb:ISRO_Mission_Control_Center
satellite deployment
ISRO Mission Control Centre
various satellite launches
|
|
gptkbp:notable_achievement
|
first Indian rocket to place a satellite in geostationary orbit
|
|
gptkbp:notable_achievements
|
launching GSAT-6 A
|
|
gptkbp:notable_launches
|
gptkb:GSAT-6_A
|
|
gptkbp:notable_mission
|
gptkb:GSAT_series
gptkb:GSAT_series_satellites
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:orbital_altitude
|
geosynchronous transfer orbit
|
|
gptkbp:part_of
|
gptkb:Indian_space_program
gptkb:Indian_Space_Program
|
|
gptkbp:payload_capacity
|
3.4 meters
5000 kg
2500 kg
2,500 kg to GTO
pre-launch operations
|
|
gptkbp:primary_use
|
gptkb:Space_Launch_System
|
|
gptkbp:propulsion
|
800 k N
|
|
gptkbp:public_interest
|
high due to national pride
|
|
gptkbp:reliability
|
high
|
|
gptkbp:research_and_development
|
ongoing improvements
|
|
gptkbp:specification
|
detailed engineering data
|
|
gptkbp:success_rate
|
approximately 80%
|
|
gptkbp:successor
|
gptkb:GSLV_Mk_III
|
|
gptkbp:supports
|
integrated launch vehicle
|
|
gptkbp:upgrades
|
enhanced payload capacity
GSLV Mk II and Mk III
|
|
gptkbp:used_for
|
launching satellites
|
|
gptkbp:weight
|
420 tons
|
|
gptkbp:bfsParent
|
gptkb:GSLV_Cryogenic_Upper_Stage_(GCU)
|
|
gptkbp:bfsLayer
|
6
|