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gptkbp:instance_of
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gptkb:Space_Launch_System
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gptkbp:collaboration
|
multiple countries
|
|
gptkbp:configuration
|
gptkb:PSLV-CA
gptkb:PSLV-DL
gptkb:PSLV-XL
PSLV-QL
XL configuration
XL variant
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:country
|
gptkb:India
|
|
gptkbp:country_of_origin
|
gptkb:India
|
|
gptkbp:debut
|
gptkb:PSLV-C1
gptkb:PSLV-C49
Over 50 successful launches
successful launches since 1994
|
|
gptkbp:design
|
10 years
|
|
gptkbp:diameter
|
2.8 meters
|
|
gptkbp:elevation
|
44 meters
2.8 meters
320 tons
|
|
gptkbp:engine_type
|
solid and liquid
Solid and liquid
|
|
gptkbp:first_flight
|
gptkb:2008
|
|
gptkbp:fuel_type
|
hypergolic and solid propellants
|
|
gptkbp:guidance_system
|
gptkb:navigation_system
|
|
gptkbp:height
|
44 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PSLV-XL
|
|
gptkbp:launch_date
|
gptkb:Annual
gptkb:2023
multiple times a year
October 15, 2008
|
|
gptkbp:launch_mass
|
320 tons
|
|
gptkbp:launch_platform
|
gptkb:ISRO_Telemetry,_Tracking_and_Command_Network
|
|
gptkbp:launch_price
|
gptkb:Low
approximately $15 million
|
|
gptkbp:launch_site
|
gptkb:Satish_Dhawan_Space_Centre
|
|
gptkbp:launch_vehicle
|
gptkb:PSLV
four stages
expendable launch vehicle
XL configuration
|
|
gptkbp:launch_window
|
varies by mission
|
|
gptkbp:launched
|
over 50
|
|
gptkbp:manufacturer
|
gptkb:Indian_Space_Research_Organisation
|
|
gptkbp:mission
|
high success rate
polar orbit insertion
|
|
gptkbp:mission_duration
|
varies by mission
|
|
gptkbp:notable_achievement
|
first Indian satellite to Mars
|
|
gptkbp:notable_achievements
|
First Asian to reach Mars orbit
Launch of 104 satellites in a single mission.
|
|
gptkbp:notable_launches
|
gptkb:Cartosat_series
gptkb:Chandrayaan-1
gptkb:space_mission
gptkb:RISAT_series
|
|
gptkbp:notable_mission
|
gptkb:space_mission
|
|
gptkbp:number_of_engines
|
gptkb:9
|
|
gptkbp:number_of_stages
|
gptkb:4
|
|
gptkbp:operational_since
|
gptkb:1994
|
|
gptkbp:operational_status
|
Active
|
|
gptkbp:orbital_inclination
|
97.5 degrees
|
|
gptkbp:payload_capacity
|
gptkb:IRNSS_satellites
3.5 meters
1,500 kg
2.8 meters
1,750 kg to Sun-synchronous orbit
1,750 kg
integrated at launch site
multiple payloads in one mission
|
|
gptkbp:primary_use
|
Scientific missions
Satellite deployment
|
|
gptkbp:primary_user
|
gptkb:ISRO
|
|
gptkbp:production_status
|
operational
|
|
gptkbp:propulsion
|
500 k N
|
|
gptkbp:release_country
|
gptkb:Yes
|
|
gptkbp:reliability
|
high
Very high
|
|
gptkbp:reusable_components
|
no
|
|
gptkbp:success_rate
|
gptkb:High
over 90%
|
|
gptkbp:used_for
|
satellite deployment
|
|
gptkbp:user
|
gptkb:Indian_government
|
|
gptkbp:bfsParent
|
gptkb:Chandrayaan-1
gptkb:space_mission
|
|
gptkbp:bfsLayer
|
4
|