|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:combustor_type
|
staged combustion
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:designed_by
|
gptkb:Space_X
|
|
gptkbp:development
|
gptkb:2002
|
|
gptkbp:development_cost
|
$30 million
|
|
gptkbp:durability
|
reusable
|
|
gptkbp:engine
|
gas-generator cycle
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:first_flight
|
gptkb:2006
gptkb:Falcon_1_Flight_4
|
|
gptkbp:flight_style
|
over 100
|
|
gptkbp:fuel_type
|
gptkb:RP-1
|
|
gptkbp:has_variations
|
gptkb:3
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Merlin engine
|
|
gptkbp:inspired_by
|
gptkb:F-1_engine
|
|
gptkbp:is_tested_for
|
Space X Rocket Development and Test Facility
|
|
gptkbp:launched
|
gptkb:commercial_crew_missions
gptkb:NASA_missions
gptkb:space_mission
gptkb:Earth_observation
international missions
satellite constellations
deep space missions
crewed missions
interplanetary missions
commercial satellites
space station missions
resupply missions
payload delivery missions
cargo missions
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:number_of_engines
|
1 to 9
|
|
gptkbp:number_of_rooms
|
69 bar
|
|
gptkbp:number_of_stages
|
gptkb:Merlin_Vacuum
gptkb:Falcon_9_first_stage
|
|
gptkbp:operational_since
|
gptkb:2006
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:propulsion
|
18.8
845 k N
|
|
gptkbp:specific_impulse
|
282 seconds (sea level)
311 seconds (vacuum)
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
gptkb:Raptor_engine
|
|
gptkbp:type
|
gptkb:Team_Rocket
|
|
gptkbp:used_for
|
launching payloads
|
|
gptkbp:used_in
|
gptkb:Falcon_1
gptkb:Falcon_9
gptkb:Falcon_Heavy
|
|
gptkbp:variant
|
gptkb:Merlin_Vacuum
gptkb:Merlin_1_A
gptkb:Merlin_1_B
gptkb:Merlin_2
gptkb:Merlin_1_C
|
|
gptkbp:weight
|
450 kg
|
|
gptkbp:bfsParent
|
gptkb:Falcon_Heavy
gptkb:Space_X
gptkb:Raptor_engine
|
|
gptkbp:bfsLayer
|
4
|