Statements (154)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Space_Launch_System
|
| gptkbp:collaboration |
gptkb:none
gptkb:France gptkb:Israel gptkb:Russia limited |
| gptkbp:configuration |
GSLV Mk I, Mk II, Mk III
three-stage |
| gptkbp:country |
gptkb:India
|
| gptkbp:country_of_origin |
gptkb:India
|
| gptkbp:debut |
gptkb:2003
gptkb:2014 extensive |
| gptkbp:design_purpose |
to enhance payload capacity
|
| gptkbp:designed_by |
gptkb:ISRO
|
| gptkbp:developed_by |
gptkb:ISRO
|
| gptkbp:development |
gptkb:1990
1990s |
| gptkbp:development_cost |
approximately $1 billion
estimated at $1 billion |
| gptkbp:engine_type |
liquid and solid
liquid and solid propulsion Vikas engine liquid and solid fuel |
| gptkbp:first_cryogenic_flight |
gptkb:2014
|
| gptkbp:first_flight |
gptkb:2001
gptkb:2003 gptkb:2023 |
| gptkbp:first_generation |
gptkb:GSLV_Mk_III
|
| gptkbp:first_gslvflight |
gptkb:GSLV-D1
|
| gptkbp:first_gtolaunch |
gptkb:GSAT-1
|
| gptkbp:flight_style |
over 20
15+ |
| gptkbp:form |
gptkb:Geosynchronous_Satellite_Launch_Vehicle
|
| gptkbp:future_plans |
upgrades and enhancements
upgraded versions |
| gptkbp:has_variations |
three
|
| gptkbp:height |
49 meters
|
| gptkbp:historical_achievement |
first successful flight in 2003
GSLV Mk II introduction in 2005 GSLV Mk III introduction in 2014 GSLV Mk III successful flight in 2017 GSLV Mk III used for Chandrayaan-2 mission GSLV Mk III used for GSAT-1 mission GSLV Mk III used for GSAT-10 mission GSLV Mk III used for GSAT-11 mission GSLV Mk III used for GSAT-12 mission GSLV Mk III used for GSAT-13 mission GSLV Mk III used for GSAT-14 mission GSLV Mk III used for GSAT-15 mission GSLV Mk III used for GSAT-16 mission GSLV Mk III used for GSAT-17 mission GSLV Mk III used for GSAT-18 mission GSLV Mk III used for GSAT-19 mission GSLV Mk III used for GSAT-2 mission GSLV Mk III used for GSAT-20 mission GSLV Mk III used for GSAT-29 mission GSLV Mk III used for GSAT-3 mission GSLV Mk III used for GSAT-30 mission GSLV Mk III used for GSAT-31 mission GSLV Mk III used for GSAT-4 mission GSLV Mk III used for GSAT-5 mission GSLV Mk III used for GSAT-6 mission GSLV Mk III used for GSAT-7 mission GSLV Mk III used for GSAT-8 mission GSLV Mk III used for GSAT-9 mission GSLV Mk III used for Gaganyaan mission GSLV Mk III used for Mangalyaan mission GSLV Mk IIIB introduction in 2017 first commercial launch in 2014 first flight in 2001 first successful cryogenic flight in 2014 |
| https://www.w3.org/2000/01/rdf-schema#label |
GSLV
|
| gptkbp:international_recognition |
recognized globally
|
| gptkbp:key_concept |
cryogenic upper stage
|
| gptkbp:key_feature |
cryogenic upper stage
|
| gptkbp:key_people |
gptkb:Indian_government
|
| gptkbp:latest_version |
gptkb:GSLV_Mk_II
|
| gptkbp:launch_date |
annual
September 2014 2-3 launches per year approximately 1-2 per year several per year |
| gptkbp:launch_event |
around 80%
multiple successful missions |
| gptkbp:launch_platform |
gptkb:ISRO
|
| gptkbp:launch_price |
$30 million
approximately $20 million |
| gptkbp:launch_site |
gptkb:Satish_Dhawan_Space_Centre
|
| gptkbp:launch_vehicle |
gptkb:Space_Launch_System
gptkb:GSLV_family modular design medium-lift detailed specifications available S139 ongoing development efforts |
| gptkbp:launched |
over 20
up to 5,000 kg to GTO three-stage |
| gptkbp:manufacturer |
gptkb:ISRO
gptkb:Indian_Space_Research_Organisation gptkb:HAL |
| gptkbp:notable_achievement |
first Indian cryogenic engine
|
| gptkbp:notable_feature |
cryogenic upper stage
geosynchronous orbit capability |
| gptkbp:notable_launches |
gptkb:GSAT-6_A
gptkb:IRNSS_satellites gptkb:INSAT_series gptkb:GSAT_series gptkb:GSAT_series_satellites |
| gptkbp:notable_mission |
gptkb:GSAT_series
GSAT series launches |
| gptkbp:number_of_stages |
gptkb:3
gptkb:Team_Rocket gptkb:GSLV_Cryogenic_Upper_Stage_(GCU) 3 stages liquid core stage liquid upper stage |
| gptkbp:operational_since |
gptkb:2001
|
| gptkbp:operational_status |
active
|
| gptkbp:operational_use |
national security and communication
|
| gptkbp:payload_capacity |
2,500 kg
5,000 kg 5000 kg to GTO up to 5,000 kg to GTO 4-meter diameter 5000 kg to geosynchronous transfer orbit |
| gptkbp:primary_use |
geostationary satellites
launching satellites into geostationary orbit launching communication satellites |
| gptkbp:primary_user |
gptkb:Indian_government
commercial clients |
| gptkbp:purpose |
gptkb:Space_Launch_System
|
| gptkbp:release_country |
no
|
| gptkbp:reliability |
high
moderate |
| gptkbp:significant_event |
GSLV D5 success
GSLV Mk III maiden flight |
| gptkbp:success_rate |
80%
approximately 80% |
| gptkbp:successor |
gptkb:GSLV_Mk_III
|
| gptkbp:technology |
indigenous
indigenous technology |
| gptkbp:type |
gptkb:Geosynchronous_Satellite_Launch_Vehicle
|
| gptkbp:used_for |
satellite launches
geostationary satellite launch |
| gptkbp:user_countries |
India only
|
| gptkbp:uses |
liquid and solid propulsion
liquid and solid propellants |
| gptkbp:bfsParent |
gptkb:ISRO
gptkb:Indian_Space_Research_Organisation gptkb:Indian_Space_Research_Organisation_(ISRO) gptkb:satellite |
| gptkbp:bfsLayer |
4
|