|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:aircraft_operated
|
up to 30 days
|
|
gptkbp:budget
|
estimated at $1 billion
|
|
gptkbp:capacity
|
up to 5,500 kg
|
|
gptkbp:collaboration
|
potential partnerships with other space agencies
|
|
gptkbp:communication_system
|
high-data-rate communication
|
|
gptkbp:community_outreach
|
engagement with educational institutions
|
|
gptkbp:contract
|
gptkb:NASA_Commercial_Resupply_Services
|
|
gptkbp:control_system
|
fly-by-wire system
|
|
gptkbp:cooling_system
|
ablative heat shield
|
|
gptkbp:crew
|
gptkb:launch_escape_system
|
|
gptkbp:crew_capacity
|
up to 7 crew members
|
|
gptkbp:design
|
completed
lifting body
modular components for easy upgrades
|
|
gptkbp:designed_by
|
gptkb:Sierra_Nevada_Corporation
|
|
gptkbp:durability
|
reusable
|
|
gptkbp:environmental_concerns
|
gptkb:health_services
|
|
gptkbp:facilities
|
gptkb:NASA's_Armstrong_Flight_Research_Center
|
|
gptkbp:first_flight
|
gptkb:2023
planned for 2023
suborbital and orbital missions
|
|
gptkbp:future_prospects
|
potential crewed missions
|
|
gptkbp:has_programs
|
gptkb:NASA's_Commercial_Crew_Program
|
|
gptkbp:height
|
3.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Dream Chaser Spacecraft
|
|
gptkbp:inspiration
|
inspired by the Space Shuttle
|
|
gptkbp:integration
|
integrated with the Atlas V rocket
|
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:landing_distance
|
runway landing
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:launch_date
|
gptkb:2023
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launch_vehicle
|
gptkb:Atlas_V
|
|
gptkbp:launched
|
planned for multiple missions
|
|
gptkbp:length
|
9.3 meters
|
|
gptkbp:media_coverage
|
extensive media coverage during development
|
|
gptkbp:mission
|
planned for lunar and Mars missions
|
|
gptkbp:mission_type
|
cargo resupply missions
|
|
gptkbp:operational_status
|
in development
|
|
gptkbp:partnerships
|
collaborations with private companies
|
|
gptkbp:payload_capacity
|
up to 3,000 kg to ISS
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:production_location
|
gptkb:Louisville,_Colorado
|
|
gptkbp:project
|
ongoing
|
|
gptkbp:propulsion
|
liquid rocket engines
|
|
gptkbp:public_interest
|
high interest from space enthusiasts
|
|
gptkbp:purpose
|
cargo transport
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:safety_record
|
aims for high safety standards
|
|
gptkbp:speed
|
controlled descent
|
|
gptkbp:sustainability
|
designed for minimal environmental impact
|
|
gptkbp:upgrades
|
planned enhancements for future missions
|
|
gptkbp:was_a_demonstration_of
|
demonstrates advanced space technologies
|
|
gptkbp:weight
|
approximately 2,500 kg
|
|
gptkbp:wingspan
|
7.3 meters
|
|
gptkbp:bfsParent
|
gptkb:Sierra_Nevada_Corporation_Space_Development
gptkb:Sierra_Nevada_Corporation_Spacecraft_Solutions_Engineering
|
|
gptkbp:bfsLayer
|
5
|