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gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:application
|
runway landing
|
|
gptkbp:armament
|
ablative
|
|
gptkbp:basedOn
|
gptkb:HL-20_Personnel_Launch_System
|
|
gptkbp:canReturnCargo
|
yes
|
|
gptkbp:canReturnCrew
|
yes
|
|
gptkbp:capacity
|
5,500 kg
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:designedFor
|
gptkb:International_Space_Station
|
|
gptkbp:duration
|
up to 210 days docked
|
|
gptkbp:firstCargoMission
|
gptkb:Tenacity
|
|
gptkbp:firstCargoMissionPlanned
|
2024
|
|
gptkbp:firstFlight
|
2024
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Dream Chaser
|
|
gptkbp:intendedUse
|
crewed spaceflight
cargo resupply
|
|
gptkbp:launchSite
|
gptkb:Cape_Canaveral_Space_Launch_Complex_41
|
|
gptkbp:launchVehicle
|
gptkb:Atlas_V
gptkb:Vulcan_Centaur
|
|
gptkbp:length
|
9 meters
|
|
gptkbp:manufacturer
|
gptkb:Sierra_Space
gptkb:Sierra_Nevada_Corporation
|
|
gptkbp:mass
|
11,000 kg
|
|
gptkbp:NASAContract
|
gptkb:Commercial_Resupply_Services_2
|
|
gptkbp:propulsion
|
hybrid rocket engines
|
|
gptkbp:reusable
|
reusable
|
|
gptkbp:seatingCapacity
|
up to 7
|
|
gptkbp:status
|
in development
|
|
gptkbp:wingspan
|
7 meters
|
|
gptkbp:bfsParent
|
gptkb:Sierra_Nevada_Corporation
|
|
gptkbp:bfsLayer
|
5
|