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gptkbp:instance_of
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gptkb:Space_Launch_System
|
|
gptkbp:collaboration
|
international space agencies
|
|
gptkbp:configuration
|
gptkb:PSLV-QP
gptkb:PSLV-CA
gptkb:PSLV-DL
gptkb:PSLV-XL
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:debut
|
gptkb:2001
over 50 successful launches
|
|
gptkbp:developed_by
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gptkb:Indian_Space_Research_Organisation_(ISRO)
|
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gptkbp:development
|
gptkb:1980s
|
|
gptkbp:diameter
|
2.8 meters
|
|
gptkbp:engine_type
|
Vikas engine
|
|
gptkbp:first_flight
|
February 2023
September 20, 1993
|
|
gptkbp:guidance_system
|
gptkb:navigation_system
|
|
gptkbp:has_role
|
gptkb:space_mission
gptkb:Earth_observation
interplanetary missions
communication satellites
|
|
gptkbp:height
|
44 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Polar Satellite Launch Vehicle (PSLV)
|
|
gptkbp:launch_date
|
multiple launches per year
|
|
gptkbp:launch_platform
|
ISRO Telemetry, Tracking and Command Network (ISTRAC)
|
|
gptkbp:launch_price
|
approximately $15 million
|
|
gptkbp:launch_site
|
gptkb:Satish_Dhawan_Space_Centre
|
|
gptkbp:launch_vehicle
|
gptkb:PSLV_family
expendable launch vehicle
|
|
gptkbp:notable_achievements
|
launching 104 satellites in a single mission
|
|
gptkbp:notable_mission
|
gptkb:Chandrayaan-1
gptkb:PSLV-C37
gptkb:space_mission
|
|
gptkbp:number_of_stages
|
gptkb:Team_Rocket
solid rocket motor
4 stages
liquid propulsion system
|
|
gptkbp:operational_since
|
gptkb:1993
|
|
gptkbp:payload_capacity
|
up to 1,750 kg to Sun-synchronous orbit
4-meter diameter
|
|
gptkbp:purpose
|
launching satellites into polar orbits
|
|
gptkbp:release_country
|
yes
|
|
gptkbp:reliability
|
one of the most reliable launch vehicles
|
|
gptkbp:success_rate
|
high
|
|
gptkbp:successor
|
GSLV (Geosynchronous Satellite Launch Vehicle)
|
|
gptkbp:user
|
gptkb:Indian_government
commercial customers
|
|
gptkbp:bfsParent
|
gptkb:Chandrayaan-1
|
|
gptkbp:bfsLayer
|
4
|