|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:air_traffic_control
|
fly-by-wire
|
|
gptkbp:aircraft_operated
|
approximately 10 days
up to 10 days
|
|
gptkbp:capacity
|
up to 7 crew members
|
|
gptkbp:cargo_capacity
|
up to 500 kg
|
|
gptkbp:cargo_types
|
return experiments and supplies
|
|
gptkbp:collaboration
|
with ESA
with ESA and other agencies
|
|
gptkbp:communication_system
|
S-band and Ku-band
|
|
gptkbp:contract
|
gptkb:NASA_Commercial_Crew_Program
|
|
gptkbp:control_system
|
fly-by-wire
autonomous docking
|
|
gptkbp:controls
|
autonomous and manual
|
|
gptkbp:cooling_system
|
ablative heat shield
|
|
gptkbp:crew
|
gptkb:NASA_astronauts
gptkb:Kennedy_Space_Center
ongoing
touchscreen controls
launch abort system
NASA astronaut selection process
NASA safety standards
comfortable seating and sleeping quarters
|
|
gptkbp:crew_capacity
|
gptkb:7
|
|
gptkbp:data_return
|
parachute landing
|
|
gptkbp:debut
|
multiple test flights
|
|
gptkbp:design
|
gptkb:United_Launch_Alliance
Boeing engineers
based on CST-100
|
|
gptkbp:designed_by
|
gptkb:Boeing
|
|
gptkbp:developed_by
|
gptkb:Boeing
|
|
gptkbp:development_cost
|
approximately $4.5 billion
$4.2 billion
|
|
gptkbp:dock_with
|
gptkb:International_Space_Station
|
|
gptkbp:durability
|
yes
up to 10 missions
|
|
gptkbp:emergency_services
|
yes
land on solid ground
|
|
gptkbp:environmental_impact
|
vibration and thermal vacuum tests
|
|
gptkbp:first_flight
|
gptkb:OFT-1
gptkb:2019
gptkb:OFT-2
gptkb:Orbital_Flight_Test_1
December 2019
scheduled for 2024
planned for 2023
uncrewed mission
OFT-1 in December 2019
OFT-2 in 2022
|
|
gptkbp:height
|
4.5 m
approximately 15 feet
|
|
gptkbp:historical_significance
|
part of the new era of space travel.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Starliner
|
|
gptkbp:integration
|
with ISS systems
|
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:is_a_supporter_of
|
educational outreach events
|
|
gptkbp:is_tested_for
|
ongoing
|
|
gptkbp:landing_distance
|
parachute and airbag
|
|
gptkbp:launch_date
|
delayed
up to 2 missions per year
up to 6 per year
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launch_vehicle
|
gptkb:Atlas_V
|
|
gptkbp:launch_window
|
varies based on ISS schedule
|
|
gptkbp:length
|
approximately 16.5 feet
4.56 m
|
|
gptkbp:life_support_system
|
advanced life support
recycling air and water
|
|
gptkbp:manufacturer
|
gptkb:Boeing
|
|
gptkbp:media_coverage
|
extensive
|
|
gptkbp:mission
|
gptkb:Houston,_Texas
located at Johnson Space Center
to ISS
commercial and government missions
data review and system checks
|
|
gptkbp:mission_type
|
low Earth orbit
|
|
gptkbp:navigation_system
|
GPS and inertial navigation
|
|
gptkbp:orbital_altitude
|
approximately 400 km
approximately 200 miles
|
|
gptkbp:part_of
|
gptkb:NASA's_Artemis_program
gptkb:Commercial_Crew_Program
|
|
gptkbp:partnership
|
gptkb:United_Launch_Alliance
gptkb:NASA
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:project
|
gptkb:advanced_propulsion_systems
|
|
gptkbp:propulsion
|
hypergolic propellants
|
|
gptkbp:public_interest
|
high
high due to space exploration goals
|
|
gptkbp:purpose
|
crew transportation
crew transport
|
|
gptkbp:recovery_method
|
land on solid ground
|
|
gptkbp:regulatory_compliance
|
FAA and NASA certifications
|
|
gptkbp:safety_features
|
gptkb:launch_escape_system
multiple redundancy
|
|
gptkbp:safety_rating
|
NASA certified
|
|
gptkbp:status
|
in development
|
|
gptkbp:supply_chain
|
multiple aerospace suppliers
|
|
gptkbp:training
|
several months for astronauts
|
|
gptkbp:training_programs
|
Boeing's Houston facility
|
|
gptkbp:updates
|
regular system upgrades
|
|
gptkbp:upgrades
|
planned for enhanced capabilities
|
|
gptkbp:weight
|
approximately 13,000 kg
approximately 13,000 pounds
|
|
gptkbp:width
|
4.2 m
approximately 15 feet
|
|
gptkbp:bfsParent
|
gptkb:NASA
|
|
gptkbp:bfsLayer
|
3
|