|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Halo_Wars_2
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
|
|
gptkbp:application
|
hypersonic flight
hypersonic travel
|
|
gptkbp:average_temperature
|
up to 1,500 ° C
|
|
gptkbp:benefits
|
reduced weight compared to rockets
|
|
gptkbp:challenges
|
thermal management
|
|
gptkbp:collaborations
|
gptkb:UK_Space_Agency
|
|
gptkbp:cooling_system
|
air-breathing
|
|
gptkbp:design
|
sustainable flight
|
|
gptkbp:developed_by
|
gptkb:Rolls-Royce
|
|
gptkbp:developer
|
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
scramjet
|
|
gptkbp:game_components
|
gptkb:Airport
gptkb:Company
gptkb:Footballer
gptkb:Photographer
gptkb:earthquake
gptkb:military_base
gptkb:Cloud_Computing_Service
gptkb:toy
gptkb:starship
gptkb:engine
gptkb:park
gptkb:railway_station
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
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SABER engine
|
|
gptkbp:innovation
|
combined cycle engine technology
|
|
gptkbp:invention
|
gptkb:SABER_1
|
|
gptkbp:is_designed_for
|
gptkb:aircraft
|
|
gptkbp:is_tested_for
|
gptkb:UK
ground testing
|
|
gptkbp:is_used_for
|
space access
|
|
gptkbp:key
|
high efficiency at various speeds
|
|
gptkbp:length
|
3.5 meters
|
|
gptkbp:part_of
|
SABER program
|
|
gptkbp:partnership
|
gptkb:aircraft
|
|
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:engine
|
|
gptkbp:weight
|
approximately 1,000 kg
|
|
gptkbp:year
|
2025
|