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gptkbp:instance_of
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gptkb:Team_Rocket
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gptkbp:application
|
satellite launches
cargo resupply missions
crew missions
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|
gptkbp:average_temperature
|
-250 to 1500 ° C
|
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gptkbp:collaboration
|
gptkb:US_Air_Force
gptkb:NASA
commercial partners
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|
gptkbp:configuration
|
gptkb:Merlin_Vacuum
gptkb:Merlin_1_A
gptkb:Merlin_1_B
gptkb:Merlin_2
gptkb:Merlin_1_D
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|
gptkbp:cooling_system
|
film cooling
|
|
gptkbp:development
|
gptkb:2002
|
|
gptkbp:development_cost
|
estimated $10 million
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:engine
|
gas-generator cycle
|
|
gptkbp:environmental_impact
|
lower emissions than predecessors
|
|
gptkbp:first_flight
|
gptkb:2006
|
|
gptkbp:fuel_type
|
gptkb:RP-1
|
|
gptkbp:future_plans
|
upgraded versions
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Space X Merlin
|
|
gptkbp:ignition_system
|
gptkb:spark_plug
|
|
gptkbp:influenced_by
|
historical rocket engines
|
|
gptkbp:inspiration
|
NASA's F-1 engine
|
|
gptkbp:invention
|
multiple patents filed
|
|
gptkbp:key_people
|
gptkb:Elon_Musk
gptkb:Gwynne_Shotwell
gptkb:Tom_Mueller
|
|
gptkbp:launched
|
over 100
|
|
gptkbp:length
|
2.5 m
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:notable_feature
|
reusable
|
|
gptkbp:number_of_engines
|
1 to 9
|
|
gptkbp:number_of_rooms
|
1000 psi
|
|
gptkbp:number_of_stages
|
gptkb:Falcon_9_first_stage
gptkb:Falcon_9_second_stage
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:part_of
|
Space X launch vehicles
|
|
gptkbp:propulsion
|
18:1
845 k N
|
|
gptkbp:public_perception
|
widely regarded as innovative
|
|
gptkbp:reliability
|
high
|
|
gptkbp:specific_impulse
|
282 seconds
|
|
gptkbp:successor
|
gptkb:Raptor_engine
|
|
gptkbp:type
|
gptkb:Team_Rocket
|
|
gptkbp:used_in
|
gptkb:Falcon_1
gptkb:Falcon_9
gptkb:Falcon_Heavy
|
|
gptkbp:weight
|
450 kg
|
|
gptkbp:bfsParent
|
gptkb:AR1_rocket_engine
|
|
gptkbp:bfsLayer
|
6
|