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gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:air_traffic_control
|
autonomous and manual control
|
|
gptkbp:cargo_capacity
|
up to 500 kg
|
|
gptkbp:collaboration
|
collaborating with international space agencies
|
|
gptkbp:communication_system
|
radio frequency communication
|
|
gptkbp:control_system
|
fly-by-wire
|
|
gptkbp:crew
|
ongoing
|
|
gptkbp:crew_capacity
|
gptkb:7
|
|
gptkbp:crew_interface
|
touchscreen displays
|
|
gptkbp:crew_selection
|
NASA astronaut selection process
|
|
gptkbp:design
|
based on CST-100 design
|
|
gptkbp:development_cost
|
approximately $4.5 billion
|
|
gptkbp:docking_system
|
NASA Docking System
|
|
gptkbp:emergency_services
|
abort system
|
|
gptkbp:expected_service_life
|
15 years
|
|
gptkbp:first_flight
|
gptkb:2019
|
|
gptkbp:fuel_type
|
hypergolic propellants
|
|
gptkbp:future_missions
|
planned for future missions to ISS
|
|
gptkbp:has_programs
|
gptkb:Commercial_Crew_Program
|
|
gptkbp:height
|
approximately 4.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Starliner spacecraft
|
|
gptkbp:integration_site
|
Boeing's facility in Florida
|
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:landing_distance
|
parachute and airbag system
|
|
gptkbp:launch_date
|
scheduled for 2023
|
|
gptkbp:launch_platform
|
gptkb:United_Launch_Alliance
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launch_vehicle
|
gptkb:Atlas_V
|
|
gptkbp:launch_window
|
determined by ISS schedule
|
|
gptkbp:length
|
approximately 4.56 meters
|
|
gptkbp:life_support_system
|
environmental control and life support system
|
|
gptkbp:manufacturer
|
gptkb:Boeing
|
|
gptkbp:mission
|
gptkb:NASA's_Johnson_Space_Center
|
|
gptkbp:operational_use
|
transport astronauts to ISS
|
|
gptkbp:part_of
|
gptkb:NASA's_Commercial_Crew_Program
|
|
gptkbp:power_source
|
batteries
|
|
gptkbp:public_interest
|
high public interest
|
|
gptkbp:purpose
|
crew transportation
|
|
gptkbp:reentry_system
|
gptkb:shield
|
|
gptkbp:safety_features
|
multiple redundancy systems
|
|
gptkbp:safety_measures
|
undergoing safety certification process
|
|
gptkbp:second_uncrewed_flight
|
gptkb:2022
|
|
gptkbp:software_system
|
custom flight software
|
|
gptkbp:solar_panels
|
deployable
|
|
gptkbp:status
|
in development
|
|
gptkbp:test_flight
|
gptkb:OFT-1
gptkb:OFT-2
uncrewed test flight
|
|
gptkbp:testing_phase
|
currently in testing phase
|
|
gptkbp:thermal_protection_system
|
ablative heat shield
|
|
gptkbp:weight
|
approximately 13,000 pounds
|
|
gptkbp:width
|
approximately 4.57 meters
|
|
gptkbp:bfsParent
|
gptkb:Commercial_Crew_Program
gptkb:Boeing
|
|
gptkbp:bfsLayer
|
4
|