Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:rocket
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:H-IIA_204
|
| gptkbp:application |
gptkb:spacecraft
|
| gptkbp:check_in_time |
150 seconds
|
| gptkbp:controls |
electronic control system
|
| gptkbp:cooling_system |
regenerative cooling
|
| gptkbp:developer |
gptkb:China
|
| gptkbp:diameter |
1.5 meters
|
| gptkbp:emissions_standard |
bell nozzle
|
| gptkbp:engine |
gptkb:musical
|
| gptkbp:engine_type |
staged combustion engine
|
| gptkbp:first_flight |
gptkb:1994
|
| gptkbp:fuel_capacity |
high
|
| gptkbp:fuel_type |
Gas-generator cycle
Liquid oxygen and kerosene |
| https://www.w3.org/2000/01/rdf-schema#label |
LE-5 B engine
|
| gptkbp:launched |
over 50
|
| gptkbp:length |
3.5 meters
|
| gptkbp:manufacturer |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:number_of_rooms |
6.5 M Pa
|
| gptkbp:propulsion |
300 seconds
120 k N |
| gptkbp:reliability |
high
|
| gptkbp:social_structure |
Liquid oxygen
|
| gptkbp:status |
in service
|
| gptkbp:succeeded_by |
95%
|
| gptkbp:used_in |
gptkb:Long_March_3_B
|
| gptkbp:weight |
800 kg
|