|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:can_be_configured_for
|
payload delivery
support payloads
|
|
gptkbp:control_system
|
gptkb:ground
|
|
gptkbp:designed_by
|
gptkb:Korea_Aerospace_Research_Institute
safety features
|
|
gptkbp:developed_by
|
gptkb:Korea_Aerospace_Research_Institute
Korean space exploration
|
|
gptkbp:development
|
gptkb:KSLV_program
|
|
gptkbp:diameter
|
3.0 meters
|
|
gptkbp:durability
|
launch environment
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:first_flight
|
gptkb:2010
gptkb:2013
|
|
gptkbp:fuel_type
|
kerosene
|
|
gptkbp:has_oxidizer_type
|
liquid oxygen
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
KSLV-1 second stage
|
|
gptkbp:is_compatible_with
|
gptkb:KSLV-1_first_stage
|
|
gptkbp:is_configured_for_testing
|
performance metrics
|
|
gptkbp:is_critical_for
|
launch success
|
|
gptkbp:is_designed_for
|
Korean satellite program
|
|
gptkbp:is_designed_to
|
reach orbit
|
|
gptkbp:is_equipped_with
|
gptkb:sensors
|
|
gptkbp:is_evaluated_by
|
gptkb:engineers
reliability
|
|
gptkbp:is_evaluated_for_cost
|
development budget
|
|
gptkbp:is_evaluated_for_performance_metrics
|
thrust and efficiency
|
|
gptkbp:is_followed_by
|
gptkb:KSLV-1_third_stage
|
|
gptkbp:is_integrated_with
|
gptkb:Space_Launch_System
gptkb:KSLV-1_first_stage
navigation systems
|
|
gptkbp:is_optimized_for
|
efficiency
|
|
gptkbp:is_part_of
|
gptkb:KSLV_program
|
|
gptkbp:is_part_of_engineering
|
KSLV-1 development
|
|
gptkbp:is_part_of_engineering_team
|
gptkb:Korea_Aerospace_Research_Institute
|
|
gptkbp:is_part_of_launch
|
KSLV-1 launch
|
|
gptkbp:is_part_of_mission_profile
|
gptkb:KSLV-1_mission
|
|
gptkbp:is_subject_to
|
regulatory approval
|
|
gptkbp:is_tested_for
|
gptkb:performance
gptkb:Korea_Test_Facility
design specifications
various conditions
static fire tests
simulated payloads
|
|
gptkbp:is_tested_for_performance
|
thrust-to-weight ratio
|
|
gptkbp:is_tested_for_stability
|
aerodynamic forces
|
|
gptkbp:is_used_for
|
orbital insertion
|
|
gptkbp:is_used_in
|
gptkb:Space_Launch_System
|
|
gptkbp:is_used_in_analysis
|
flight dynamics
|
|
gptkbp:is_used_in_design
|
gptkb:KSLV-1_rocket
|
|
gptkbp:is_used_in_launch
|
KSLV-1 missions
|
|
gptkbp:is_used_in_testing
|
flight tests
|
|
gptkbp:launch_vehicle
|
gptkb:KSLV-1
|
|
gptkbp:launched
|
gptkb:Naro_Space_Center
|
|
gptkbp:launched_in
|
gptkb:KSLV-1_first_stage
|
|
gptkbp:length
|
10.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Korea_Aerospace_Industries
|
|
gptkbp:mass
|
1,500 kg
|
|
gptkbp:mission
|
gptkb:Naro-1
Korean satellite launch
|
|
gptkbp:operates_in
|
outer space
|
|
gptkbp:part_of
|
gptkb:KSLV-1
|
|
gptkbp:propulsion
|
30 k N
|
|
gptkbp:safety_rating
|
launch conditions
|
|
gptkbp:successor
|
gptkb:KSLV-2
|
|
gptkbp:system
|
gptkb:KSLV_launch_system
|
|
gptkbp:uses_propellant
|
gptkb:RP-1
liquid oxygen
|
|
gptkbp:bfsParent
|
gptkb:Korea_Space_Launch_Vehicle_(KSLV)
|
|
gptkbp:bfsLayer
|
6
|