|
gptkbp:instanceOf
|
rocket engine
|
|
gptkbp:application
|
gptkb:Apollo_program
|
|
gptkbp:barrelLength
|
70 psi
|
|
gptkbp:bombLoad
|
bell nozzle
|
|
gptkbp:chemicalFormula
|
Liquid Oxygen
|
|
gptkbp:construction_cost
|
$18 million
|
|
gptkbp:coolingSystem
|
regenerative cooling
film cooling
|
|
gptkbp:design
|
50 missions
|
|
gptkbp:designedBy
|
Rocketdyne
|
|
gptkbp:developer
|
1955 to 1967
|
|
gptkbp:diameter
|
12.2 ft
|
|
gptkbp:duration
|
150 seconds
|
|
gptkbp:engine
|
gptkb:California
modular
influenced future designs
start-up procedure
turbopumps
|
|
gptkbp:engineConfiguration
|
vertical
|
|
gptkbp:engineType
|
liquid bipropellant
|
|
gptkbp:facilities
|
gptkb:NASA_Marshall_Space_Flight_Center
|
|
gptkbp:firstFlight
|
1967
|
|
gptkbp:firstMatch
|
1965
|
|
gptkbp:fuel_capacity
|
2.5:1
single chamber
12,000 lb/min
|
|
gptkbp:fuelCapacity
|
RP-1
|
|
gptkbp:fuelType
|
gas-generator cycle
hypergolic
RP-1_and_Liquid_Oxygen
|
|
gptkbp:hasArea
|
gptkb:Florida
static fire tests
|
|
gptkbp:hasDepartment
|
150 seconds
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F-1 Rocket Engine
|
|
gptkbp:inspiration
|
J-2 engine
|
|
gptkbp:launchDate
|
gptkb:Apollo_missions
|
|
gptkbp:launchVehicle
|
Saturn I
|
|
gptkbp:length
|
19.5 ft
|
|
gptkbp:numberOfEpisodes
|
5
|
|
gptkbp:operational_area
|
29,000 lb/min
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operationalHistory
|
first large-scale rocket engine
|
|
gptkbp:performances
|
high
moderate
high thrust
documented in reports
detailed_in_NASA_documents
|
|
gptkbp:produces
|
15
|
|
gptkbp:propulsion
|
1,500,000 lbf
mechanical gimbal
81.1
|
|
gptkbp:related_engine
|
staged combustion
safe shut down
|
|
gptkbp:successor
|
gptkb:F-1B
|
|
gptkbp:technology
|
liquid rocket propulsion
|
|
gptkbp:usedIn
|
gptkb:Saturn_V
|
|
gptkbp:weight
|
18,500 lb
|