gptkbp:instance_of
|
gptkb:jet_engine
|
gptkbp:application
|
gptkb:business_jet
|
gptkbp:average_temperature
|
1500 K
|
gptkbp:bypass_ratio
|
8:1
|
gptkbp:certification
|
gptkb:EASA
|
gptkbp:competitors
|
gptkb:GE_Passport
|
gptkbp:compressor_type
|
gptkb:5
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
gptkbp:cooling_system
|
air-cooled
|
gptkbp:customer_support
|
gptkb:Bombardier
global network
|
gptkbp:design
|
20,000 hours
Rolls-Royce engineers
|
gptkbp:development
|
BR700 family
|
gptkbp:diameter
|
1.5 m
1.1 m
|
gptkbp:elevation
|
51,000 ft
|
gptkbp:emissions_standard
|
low
|
gptkbp:enforces
|
complies with ICAO standards
|
gptkbp:engine
|
advanced aerodynamics
state-of-the-art technology
ongoing development
air start
BR725
|
gptkbp:engine_configuration
|
modular design
twin-spool
pylon-mounted
|
gptkbp:engine_power
|
high reliability
optimized for efficiency
|
gptkbp:engine_safety
|
meets safety standards
|
gptkbp:engine_type
|
high bypass turbofan
|
gptkbp:first_flight
|
gptkb:2016
|
gptkbp:fuel_capacity
|
3,000 liters
|
gptkbp:fuel_economy
|
high
0.85 kg/k N/h
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
https://www.w3.org/2000/01/rdf-schema#label
|
BR710 A2-70
|
gptkbp:ignition_system
|
dual ignition
|
gptkbp:is_tested_for
|
extensive ground testing
|
gptkbp:length
|
3.5 m
|
gptkbp:maintenance
|
4,000 hours
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
gptkbp:market_position
|
high
|
gptkbp:market_segment
|
business aviation
|
gptkbp:max_speed
|
Mach 0.90
|
gptkbp:noise_level
|
Stage 4 compliant
|
gptkbp:operational_cost
|
competitive
|
gptkbp:power_output
|
70 k N
|
gptkbp:propulsion
|
46:1
70 k N
|
gptkbp:related_aircraft
|
gptkb:Global_7500
|
gptkbp:service_entry
|
gptkb:2018
|
gptkbp:turbine_type
|
2
|
gptkbp:type
|
gptkb:turbofan_engine
|
gptkbp:used_in
|
Bombardier Global 7000
|
gptkbp:warranty
|
5 years
|
gptkbp:weight
|
1,500 kg
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_BR710
|
gptkbp:bfsLayer
|
5
|