|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
heavy-lift launch vehicles
|
|
gptkbp:challenges
|
engine performance optimization
high thrust requirements
|
|
gptkbp:check_in_time
|
approximately 200 seconds
|
|
gptkbp:collaborations
|
various aerospace companies
|
|
gptkbp:combustor_type
|
staged combustion
|
|
gptkbp:community_engagement
|
outreach programs
|
|
gptkbp:community_impact
|
contributing to space exploration
|
|
gptkbp:competitors
|
gptkb:Space_X_Raptor_engine
|
|
gptkbp:control_system
|
advanced avionics
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:debut
|
gptkb:2017
|
|
gptkbp:design
|
multiple prototypes
|
|
gptkbp:design_philosophy
|
reusability
|
|
gptkbp:development
|
Blue Origin engineers
|
|
gptkbp:development_cost
|
estimated at $1 billion
|
|
gptkbp:educational_programs
|
STEM programs
|
|
gptkbp:engine
|
modular design
staged combustion cycle
Aerojet Rocketdyne AR1
|
|
gptkbp:engine_configuration
|
detailed technical documentation
single-shaft
|
|
gptkbp:engine_power
|
designed for multiple uses
|
|
gptkbp:environmental_impact
|
lower emissions than kerosene engines
|
|
gptkbp:exhaust_system
|
expander cycle nozzle
|
|
gptkbp:first_flight
|
gptkb:2023
|
|
gptkbp:fuel_capacity
|
1.5 m
|
|
gptkbp:fuel_economy
|
high efficiency
|
|
gptkbp:fuel_type
|
liquid natural gas
|
|
gptkbp:funding
|
private investment
|
|
gptkbp:future_plans
|
commercial launches
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Blue Origin BE-4 engine
|
|
gptkbp:ignition_system
|
dual start system
|
|
gptkbp:innovation
|
cutting-edge technology
|
|
gptkbp:inspiration
|
gptkb:NASA's_Space_Launch_System
|
|
gptkbp:investment
|
high demand for launch services
|
|
gptkbp:is_tested_for
|
gptkb:Blue_Origin's_test_facility_in_West_Texas
hot-fire testing
ongoing hot-fire tests
|
|
gptkbp:launch_cadence
|
planned for high frequency
|
|
gptkbp:launch_vehicle
|
gptkb:New_Glenn
|
|
gptkbp:manufacturer
|
gptkb:Blue_Origin
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:partnerships
|
United Launch Alliance (ULA)
|
|
gptkbp:performance
|
high performance
|
|
gptkbp:production_status
|
in development
|
|
gptkbp:project
|
ongoing development
upgraded versions planned
reliable and cost-effective launches
|
|
gptkbp:propulsion
|
approximately 2,400 k N
approximately 80:1
|
|
gptkbp:public_perception
|
positive reception
|
|
gptkbp:regulatory_compliance
|
FAA approved
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:strategic_importance
|
key to future missions
|
|
gptkbp:sustainability_efforts
|
focus on eco-friendly technologies
|
|
gptkbp:used_in
|
gptkb:New_Glenn_rocket
|
|
gptkbp:weight
|
approximately 3,000 kg
|
|
gptkbp:bfsParent
|
gptkb:AR1_rocket_engine
|
|
gptkbp:bfsLayer
|
6
|