X-33 Reusable Launch Vehicle

GPTKB entity

Predicate	Object
gptkbp:instanceOf	gptkb:technology gptkb:experimental_spacecraft
gptkbp:cancellationDate	2001 cost overruns technical difficulties failure of composite hydrogen tank
gptkbp:countryOfOrigin	gptkb:United_States
gptkbp:engineType	Linear Aerospike XRS-2200
gptkbp:firstFlight	1999
gptkbp:firstFlightLocationPlanned	gptkb:Edwards_Air_Force_Base
gptkbp:fuelType	liquid hydrogen
gptkbp:fundedBy	gptkb:NASA
gptkbp:height	7.6 m
gptkbp:intendedToDemonstrate	single-stage-to-orbit technology reusable launch vehicle technology
gptkbp:length	21.9 m
gptkbp:manufacturer	gptkb:Lockheed_Martin
gptkbp:mass	57,153 kg
gptkbp:notableProject	gptkb:public-private_partnership
gptkbp:operator	gptkb:NASA
gptkbp:oxidizer	liquid oxygen
gptkbp:plannedFlightProfile	suborbital
gptkbp:plannedLandingMethod	horizontal landing
gptkbp:plannedLaunchMethod	vertical takeoff
gptkbp:projectEndDate	2001
gptkbp:propulsion	aerospike engine
gptkbp:relatedTo	gptkb:Space_Shuttle gptkb:VentureStar gptkb:Reusable_Launch_Vehicle_program
gptkbp:startYear	1996
gptkbp:status	cancelled
gptkbp:successor	gptkb:VentureStar
gptkbp:testFlightsConducted	0
gptkbp:website	https://www.nasa.gov/centers/marshall/news/background/facts/x33.html
gptkbp:wingspan	22.9 m
gptkbp:bfsParent	gptkb:David_Urie
gptkbp:bfsLayer	8
https://www.w3.org/2000/01/rdf-schema#label	X-33 Reusable Launch Vehicle