|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:budget
|
$400 million
|
|
gptkbp:challenges
|
high
|
|
gptkbp:collaboration
|
gptkb:Russia
|
|
gptkbp:control_system
|
gptkb:navigation_system
|
|
gptkbp:country
|
gptkb:South_Korea
|
|
gptkbp:country_of_origin
|
gptkb:South_Korea
|
|
gptkbp:debut
|
gptkb:2013
recorded
|
|
gptkbp:design
|
5 years
|
|
gptkbp:developed_by
|
gptkb:Korea_Aerospace_Research_Institute
|
|
gptkbp:development
|
gptkb:2002
gptkb:2009
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
liquid fuel
|
|
gptkbp:first_flight
|
gptkb:2009
2023-10-01
|
|
gptkbp:flight_style
|
2
|
|
gptkbp:fuel_type
|
RP-1 and liquid oxygen
|
|
gptkbp:future_plans
|
Nuri rocket development
|
|
gptkbp:guidance_system
|
gptkb:GPS
|
|
gptkbp:height
|
25 meters
33 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Naro-1
|
|
gptkbp:launch_date
|
1 per year
|
|
gptkbp:launch_event
|
1 out of 2
|
|
gptkbp:launch_mass
|
140 tons
|
|
gptkbp:launch_platform
|
gptkb:Korea_Aerospace_Research_Institute
gptkb:Naro_Space_Center
|
|
gptkbp:launch_site
|
gptkb:Naro_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:KSLV_family
KSLV
|
|
gptkbp:launch_window
|
varies
|
|
gptkbp:manufacturer
|
gptkb:Korea_Aerospace_Research_Institute
Naro Space
|
|
gptkbp:mission
|
conducted
|
|
gptkbp:mission_type
|
gptkb:space_mission
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbital_inclination
|
90 degrees
|
|
gptkbp:payload_capacity
|
150 kg
2.6 meters
100 kg to low Earth orbit
|
|
gptkbp:project
|
7 years
completed
establish satellite launch capability
|
|
gptkbp:propulsion
|
300 k N
|
|
gptkbp:purpose
|
gptkb:Space_Launch_System
|
|
gptkbp:reliability
|
moderate
|
|
gptkbp:specification
|
documented
|
|
gptkbp:strategic_goals
|
technical issues
|
|
gptkbp:success_rate
|
80%
50%
|
|
gptkbp:successor
|
Nuri
|
|
gptkbp:supports
|
used
|
|
gptkbp:bfsParent
|
gptkb:KSLV-II
gptkb:KSLV-1_second_stage
gptkb:Naro_Space_Center
|
|
gptkbp:bfsLayer
|
7
|