|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:aircraft_operated
|
up to 60 days
|
|
gptkbp:avionics
|
modern digital systems
|
|
gptkbp:capacity
|
5,500 kg
|
|
gptkbp:cargo_return
|
capable of returning cargo to Earth
|
|
gptkbp:cargo_types
|
pressurized and unpressurized
|
|
gptkbp:collaboration
|
collaborating with various space agencies
|
|
gptkbp:community_engagement
|
outreach programs planned
|
|
gptkbp:contract_award
|
NASA in 2020
|
|
gptkbp:crew_capacity
|
gptkb:none
|
|
gptkbp:design
|
reusable
allows for upgrades
|
|
gptkbp:development_cost
|
estimated $1 billion
|
|
gptkbp:environmental_impact
|
minimized through design
|
|
gptkbp:first_flight
|
gptkb:2023
planned for 2024
|
|
gptkbp:future_plans
|
expanding to lunar missions
|
|
gptkbp:height
|
3.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Dream Chaser cargo variant
|
|
gptkbp:inspiration
|
gptkb:Space_Shuttle
|
|
gptkbp:integration
|
with ISS systems
|
|
gptkbp:investment_strategy
|
attracting venture capital
|
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:is_user_friendly
|
designed for easy operation
|
|
gptkbp:launch_date
|
up to 6 missions per year
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launch_vehicle
|
gptkb:Vulcan_Centaur
|
|
gptkbp:launch_window
|
flexible scheduling
|
|
gptkbp:length
|
9.3 meters
|
|
gptkbp:manufacturer
|
gptkb:Sierra_Nevada_Corporation
|
|
gptkbp:market
|
commercial spaceflight
|
|
gptkbp:media_coverage
|
significant in aerospace news
|
|
gptkbp:operational_lifetime
|
15 years
|
|
gptkbp:operational_status
|
in development
|
|
gptkbp:part_of_program
|
gptkb:NASA_Commercial_Resupply_Services
|
|
gptkbp:partnerships
|
with commercial companies
|
|
gptkbp:payload_capacity
|
up to 3,000 kg to ISS
|
|
gptkbp:projected_revenue
|
estimated $500 million annually
|
|
gptkbp:propulsion
|
liquid rocket engines
|
|
gptkbp:public_interest
|
high due to innovative design
|
|
gptkbp:purpose
|
cargo transport
|
|
gptkbp:regulatory_compliance
|
in process with FAA
|
|
gptkbp:research_applications
|
supports scientific experiments
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:safety_measures
|
meets NASA requirements
|
|
gptkbp:speed
|
glide landing
|
|
gptkbp:supporting_technologies
|
advanced robotics
|
|
gptkbp:sustainability
|
designed for multiple missions
|
|
gptkbp:thermal_protection_system
|
ablative heat shield
|
|
gptkbp:training_programs
|
for astronauts and operators
|
|
gptkbp:weight
|
approximately 3,000 kg
|
|
gptkbp:wingspan
|
7.3 meters
|
|
gptkbp:bfsParent
|
gptkb:Sierra_Nevada_Corporation's_Spacecraft_Development
|
|
gptkbp:bfsLayer
|
6
|