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gptkbp:instance_of
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gptkb:Space_Launch_System
|
|
gptkbp:collaboration
|
limited
|
|
gptkbp:configuration
|
multiple configurations available
|
|
gptkbp:designed_for
|
launching satellites into polar orbits
|
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gptkbp:development
|
gptkb:1980s
|
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gptkbp:diameter
|
2.8 meters
|
|
gptkbp:first_flight
|
gptkb:1994
|
|
gptkbp:first_generation
|
under development
|
|
gptkbp:fuel_type
|
solid and liquid propellants
|
|
gptkbp:height
|
approximately 44 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
polar launch vehicle
|
|
gptkbp:launch_date
|
multiple launches per year
|
|
gptkbp:launch_price
|
relatively low
|
|
gptkbp:launch_site
|
gptkb:Satish_Dhawan_Space_Centre
|
|
gptkbp:manufacturer
|
gptkb:Indian_Space_Research_Organisation
|
|
gptkbp:notable_feature
|
high reliability
|
|
gptkbp:notable_mission
|
IRS satellites
|
|
gptkbp:number_of_stages
|
two stages
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:payload_capacity
|
up to 1,000 kg
|
|
gptkbp:primary_use
|
gptkb:Earth_observation
|
|
gptkbp:propulsion
|
over 400 k N
|
|
gptkbp:reliability
|
above 95%
|
|
gptkbp:success_count
|
over 50 successful launches
|
|
gptkbp:success_rate
|
high
|
|
gptkbp:type
|
expendable launch vehicle
|
|
gptkbp:used_by
|
gptkb:Indian_government
|
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gptkbp:bfsParent
|
gptkb:PSLV-C37
|
|
gptkbp:bfsLayer
|
5
|