|
gptkbp:instanceOf
|
hypersonic spaceplane concept
|
|
gptkbp:countryOfOrigin
|
gptkb:Germany
|
|
gptkbp:developedBy
|
gptkb:German_Aerospace_Center_(DLR)
|
|
gptkbp:flightNumber
|
90 minutes (Europe to Australia)
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
DLR SpaceLiner
|
|
gptkbp:intendedUse
|
suborbital passenger transport
|
|
gptkbp:landingConfiguration
|
horizontal landing
|
|
gptkbp:launchConfiguration
|
vertical takeoff
|
|
gptkbp:maximumSpeed
|
Mach 25
|
|
gptkbp:notableFeature
|
liquid hydrogen/liquid oxygen engines
advanced thermal protection system
high-speed atmospheric reentry
separate passenger stage and booster stage
|
|
gptkbp:notableProject
|
Martin Sippel
|
|
gptkbp:proposedBy
|
2005
|
|
gptkbp:propulsion
|
rocket-powered
|
|
gptkbp:publiclyPresentedAt
|
gptkb:International_Astronautical_Congress
|
|
gptkbp:relatedTo
|
space tourism
reusable launch systems
point-to-point suborbital flight
|
|
gptkbp:reusable
|
reusable
|
|
gptkbp:seatingCapacity
|
2
50
|
|
gptkbp:status
|
conceptual design
|
|
gptkbp:targetMarket
|
ultra-fast intercontinental travel
|
|
gptkbp:website
|
https://www.dlr.de/
|
|
gptkbp:bfsParent
|
gptkb:Deutsches_Zentrum_für_Luft-_und_Raumfahrt_(DLR)
|
|
gptkbp:bfsLayer
|
8
|