|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:check_in_time
|
8.5 minutes
|
|
gptkbp:control_system
|
digital
fly-by-wire
|
|
gptkbp:cooling_system
|
regenerative cooling
regenerative cooling system
|
|
gptkbp:development
|
F-1 engine technology
|
|
gptkbp:durability
|
yes
|
|
gptkbp:engine
|
gptkb:NASA_Michoud_Assembly_Facility
gptkb:Space_Shuttle_missions
1970s
advanced materials
modular
staged combustion
|
|
gptkbp:engine_configuration
|
high performance
modular design
clustered
1,000,000 lbf
F-1 technology
|
|
gptkbp:engine_ignition_method
|
hypergolic ignition system
|
|
gptkbp:engine_power
|
high reliability
high efficiency
|
|
gptkbp:engine_refurbishment
|
yes
|
|
gptkbp:engine_test_facility
|
Rocketdyne test facility
|
|
gptkbp:engine_testing_method
|
static firing
|
|
gptkbp:engine_thrust_control
|
yes
|
|
gptkbp:engine_thrust_measurement
|
measured in pounds-force
|
|
gptkbp:engine_thrust_rating_per_engine
|
1,000,000 lbf
|
|
gptkbp:engine_thrust_vectoring_capability
|
yes
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:first_flight
|
gptkb:1981
gptkb:2011
|
|
gptkbp:fuel_economy
|
12,000 lb/min
|
|
gptkbp:fuel_type
|
liquid hydrogen and liquid oxygen
liquid oxygen and liquid hydrogen
|
|
gptkbp:gimbal_range
|
±8 degrees
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Space Shuttle main engines
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:investment
|
3,000 psi
|
|
gptkbp:is_tested_for
|
gptkb:NASA_Marshall_Space_Flight_Center
static fire test
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Space_Shuttle
|
|
gptkbp:manufacturer
|
gptkb:Rocketdyne
|
|
gptkbp:nozzle
|
aerospike nozzle
|
|
gptkbp:number_of_engines
|
three
|
|
gptkbp:number_of_rooms
|
single chamber
|
|
gptkbp:number_of_stages
|
orbital maneuvering system
SRB (Solid Rocket Boosters)
|
|
gptkbp:operational_use
|
up to 100 flights
|
|
gptkbp:propulsion
|
yes
1,000,000 lbf
128:1
1,000,000 lbf per engine
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:type
|
liquid-fueled
|
|
gptkbp:used_in
|
gptkb:Space_Shuttle
|
|
gptkbp:weight
|
7,800 lb
|
|
gptkbp:bfsParent
|
gptkb:NASA's_Engine_Test_Facility
gptkb:Rocketdyne_engines
|
|
gptkbp:bfsLayer
|
6
|