|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_type
|
gptkb:monoplane
|
|
gptkbp:application
|
hypersonic flight
|
|
gptkbp:average_temperature
|
up to 1,500 ° C
|
|
gptkbp:benefits
|
reduced weight compared to rockets
|
|
gptkbp:can_be_used_to
|
space access
|
|
gptkbp:challenges
|
thermal management
|
|
gptkbp:collaboration
|
gptkb:UK_Space_Agency
|
|
gptkbp:combustor_type
|
scramjet
|
|
gptkbp:components
|
gptkb:turbofan_engine
gptkb:spark_plug
gptkb:monitor
gptkb:Noldor
gptkb:Control
gptkb:Blaster
gptkb:gasoline
gptkb:apparel
gptkb:sensors
gptkb:scanner
gptkb:exhaust_system
actuators
feedback loops
diagnostic tools
safety systems
fuel lines
air intake
vibration dampers
casing
heat exchanger
valve system
emergency shutoff system
mounting brackets
control electronics
modular design features
mounting structure
control valves
thrust vector control system
maintenance access points
air ducts
cooling fins
integration points
turbofan section
|
|
gptkbp:cooling_system
|
air-breathing
|
|
gptkbp:design_purpose
|
sustainable flight
|
|
gptkbp:designed_for
|
gptkb:aircraft
|
|
gptkbp:developed_by
|
gptkb:Rolls-Royce
|
|
gptkbp:development
|
gptkb:2010
|
|
gptkbp:diameter
|
1 meter
|
|
gptkbp:elevation
|
up to 100,000 feet
|
|
gptkbp:engine
|
air-breathing cycle
|
|
gptkbp:environmental_impact
|
lower emissions than traditional rockets
|
|
gptkbp:first_flight
|
gptkb:2020
|
|
gptkbp:fuel_type
|
kerosene
|
|
gptkbp:future_application
|
hypersonic travel
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SABER engine
|
|
gptkbp:innovation
|
combined cycle engine technology
|
|
gptkbp:invention
|
gptkb:SABER_1
|
|
gptkbp:is_tested_for
|
gptkb:UK
ground testing
|
|
gptkbp:key_feature
|
high efficiency at various speeds
|
|
gptkbp:length
|
3.5 meters
|
|
gptkbp:part_of
|
SABER program
|
|
gptkbp:partnership
|
gptkb:Boeing
|
|
gptkbp:performance
|
specific impulse
|
|
gptkbp:propulsion
|
up to 25,000 lbf
|
|
gptkbp:related_to
|
gptkb:Reaction_Engines_Limited
|
|
gptkbp:research_focus
|
gptkb:advanced_propulsion_systems
|
|
gptkbp:status
|
in development
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:weight
|
approximately 1,000 kg
|
|
gptkbp:year
|
2025
|
|
gptkbp:bfsParent
|
gptkb:Halo_Wars_2
|
|
gptkbp:bfsLayer
|
5
|