Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:average_temperature |
3,000 ° F
|
| gptkbp:combustion_chamber_pressure |
3,000 psi
|
| gptkbp:designed_by |
gptkb:Rocketdyne
|
| gptkbp:development_cost |
$1 billion
|
| gptkbp:durability |
gptkb:true
|
| gptkbp:engine |
staged combustion
|
| gptkbp:engine_configuration |
liquid bipropellant
|
| gptkbp:first_flight |
gptkb:STS-1
|
| gptkbp:flight_style |
135
|
| gptkbp:fuel_capacity |
5.5 ft
14.5 ft |
| gptkbp:fuel_type |
liquid hydrogen and liquid oxygen
|
| gptkbp:has_programs |
Space Shuttle Main Engine (SSME)
|
| https://www.w3.org/2000/01/rdf-schema#label |
RS-25 B
|
| gptkbp:mission |
gptkb:NASA_missions
|
| gptkbp:number_of_engines |
four
|
| gptkbp:operational_since |
gptkb:1981
|
| gptkbp:propulsion |
190,000 lbf
|
| gptkbp:replaced_by |
gptkb:RS-25_E
|
| gptkbp:specific_impulse |
452 seconds
|
| gptkbp:used_in |
gptkb:Artemis_program
gptkb:Space_Shuttle |
| gptkbp:weight |
3,000 lb
|
| gptkbp:bfsParent |
gptkb:Rocketdyne_RS-25
|
| gptkbp:bfsLayer |
5
|