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gptkbp:instance_of
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gptkb:Space_Launch_System
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|
gptkbp:academic_programs
|
aerodynamic efficiency
|
|
gptkbp:challenges
|
overcoming technical hurdles
|
|
gptkbp:collaboration
|
gptkb:various_countries
|
|
gptkbp:community_engagement
|
outreach programs
|
|
gptkbp:country
|
gptkb:India
|
|
gptkbp:debut
|
gptkb:PSLV-C67
|
|
gptkbp:design
|
dedicated professionals
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|
gptkbp:diameter
|
2.8 meters
|
|
gptkbp:educational_value
|
inspiring students
|
|
gptkbp:environmental_impact
|
minimal
|
|
gptkbp:first_flight
|
1994-09-20
|
|
gptkbp:future_plans
|
more advanced missions
|
|
gptkbp:height
|
44 meters
|
|
gptkbp:home_ground
|
multiple locations in India
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PSLV-C66
|
|
gptkbp:innovation
|
cutting-edge technology
|
|
gptkbp:launch_broadcast
|
live coverage
|
|
gptkbp:launch_date
|
2023-10-05
frequent
2023-05-04
|
|
gptkbp:launch_event
|
high
successful
public event
|
|
gptkbp:launch_mass
|
320 tons
|
|
gptkbp:launch_platform
|
gptkb:ISRO_Telemetry,_Tracking_and_Command_Network
satellite monitoring
data evaluation
|
|
gptkbp:launch_price
|
approximately $15 million
|
|
gptkbp:launch_site
|
gptkb:Satish_Dhawan_Space_Centre
|
|
gptkbp:launch_vehicle
|
gptkb:PSLV
gptkb:polar_launch_vehicle
|
|
gptkbp:launch_window
|
specific time frame
|
|
gptkbp:launched
|
gptkb:1
gptkb:Indian_Space_Research_Organisation
several months
extensive testing
|
|
gptkbp:manufacturer
|
gptkb:ISRO
|
|
gptkbp:media_coverage
|
extensive
|
|
gptkbp:mission
|
ISRO control room
deploy satellites into orbit
|
|
gptkbp:mission_duration
|
varies by payload
|
|
gptkbp:mission_type
|
gptkb:Space_Launch_System
Satellite Launch
|
|
gptkbp:notable_achievements
|
launching Mars Orbiter Mission
|
|
gptkbp:number_of_stages
|
gptkb:4
gptkb:Team_Rocket
solid rocket motor
liquid engine
|
|
gptkbp:operator
|
gptkb:Indian_Space_Research_Organisation
|
|
gptkbp:orbit_type
|
gptkb:22
|
|
gptkbp:orbital_inclination
|
97.5 degrees
|
|
gptkbp:orbital_period
|
specific trajectory
|
|
gptkbp:payload_capacity
|
1,750 kg to Sun-synchronous orbit
complex process
multiple small satellites
GISAT
multiple orbits
|
|
gptkbp:predecessor
|
gptkb:PSLV-C65
|
|
gptkbp:project
|
upgraded versions
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:public_interest
|
high
|
|
gptkbp:recognition
|
widely respected
|
|
gptkbp:release_country
|
collaborative missions
|
|
gptkbp:reliability
|
high
|
|
gptkbp:safety_measures
|
stringent protocols
|
|
gptkbp:scientific_goals
|
earth observation
|
|
gptkbp:successor
|
gptkb:PSLV-C65
gptkb:PSLV-C67
|
|
gptkbp:tracking_systems
|
advanced telemetry systems
|
|
gptkbp:was_a_demonstration_of
|
new satellite technologies
|
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gptkbp:bfsParent
|
gptkb:PSLV-C65
|
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gptkbp:bfsLayer
|
14
|