Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Space_Launch_System
|
| gptkbp:collaboration |
gptkb:Yes
|
| gptkbp:control_system |
gptkb:navigation_system
|
| gptkbp:country |
gptkb:South_Korea
|
| gptkbp:debut |
gptkb:2013
|
| gptkbp:developed_by |
gptkb:Korea_Aerospace_Research_Institute
|
| gptkbp:development |
gptkb:2002
|
| gptkbp:engine_type |
gptkb:Team_Rocket
|
| gptkbp:first_flight |
gptkb:2009
|
| gptkbp:fuel_type |
RP-1 and liquid oxygen
|
| gptkbp:height |
33 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
KSLV launch system
|
| gptkbp:launch_date |
1-2 per year
|
| gptkbp:launch_price |
approximately $30 million
|
| gptkbp:launch_site |
gptkb:Naro_Space_Center
|
| gptkbp:manufacturer |
gptkb:Korea_Aerospace_Industries
|
| gptkbp:mass |
140 tons
|
| gptkbp:notable_launches |
STSAT-2 B
|
| gptkbp:number_of_stages |
2
|
| gptkbp:orbital_inclination |
90 degrees
|
| gptkbp:payload_capacity |
1000 kg to LEO
|
| gptkbp:purpose |
gptkb:Space_Launch_System
|
| gptkbp:reliability |
70%
|
| gptkbp:successor |
gptkb:KSLV-II
|
| gptkbp:bfsParent |
gptkb:KSLV-1_second_stage
|
| gptkbp:bfsLayer |
7
|