|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:assembly_location
|
gptkb:Palmdale,_California
|
|
gptkbp:avionics
|
advanced avionics system
|
|
gptkbp:benefits
|
cancellation
|
|
gptkbp:cancellation_reason
|
funding issues
|
|
gptkbp:collaborative_projects
|
NASA, Lockheed Martin, Boeing
|
|
gptkbp:control_system
|
fly-by-wire
|
|
gptkbp:crew_capacity
|
2
|
|
gptkbp:design
|
gptkb:Lockheed_Martin_Skunk_Works
multiple
completed
single-stage-to-orbit
|
|
gptkbp:design_features
|
delta wing
|
|
gptkbp:design_purpose
|
reduce launch costs
|
|
gptkbp:elevation
|
up to 100 km
|
|
gptkbp:engine
|
gptkb:Rocketdyne
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:first_flight
|
gptkb:1996
gptkb:3
limited
|
|
gptkbp:flight_style
|
suborbital and orbital
|
|
gptkbp:fuel_type
|
liquid hydrogen
|
|
gptkbp:funding
|
gptkb:NASA
|
|
gptkbp:fuselage_material
|
composite materials
|
|
gptkbp:ground_testing
|
extensive
|
|
gptkbp:has_programs
|
gptkb:X-33_program
gptkb:Space_Launch_Initiative
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lockheed Martin X-33
|
|
gptkbp:inspiration
|
gptkb:Space_Shuttle
|
|
gptkbp:invention
|
gptkb:1
|
|
gptkbp:is_influenced_by
|
reusable launch systems
|
|
gptkbp:landing_distance
|
runway landing
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral
|
|
gptkbp:launch_vehicle
|
not applicable
|
|
gptkbp:legacy
|
influenced future designs
paved the way for future RLVs
|
|
gptkbp:legislation
|
space exploration policy
|
|
gptkbp:length
|
82 feet (25 m)
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:max_takeoff_weight
|
150,000 pounds (68,000 kg)
|
|
gptkbp:notable_pilots
|
gptkb:Gordon_Fullerton
|
|
gptkbp:operational_use
|
not achieved
reusable spaceplane
|
|
gptkbp:orbital_capability
|
low Earth orbit
|
|
gptkbp:parent_agency
|
NASA, Lockheed Martin
|
|
gptkbp:project
|
gptkb:John_D._Mc_Gowan
5 years
1996-2001
|
|
gptkbp:projected_operational_date
|
gptkb:2000
|
|
gptkbp:purpose
|
reusable launch vehicle
|
|
gptkbp:release_date
|
1996-10-31
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:status
|
canceled
|
|
gptkbp:successor
|
X-34
|
|
gptkbp:test_vehicle
|
yes
|
|
gptkbp:was_a_demonstration_of
|
yes
|
|
gptkbp:weight
|
40,000 pounds (18,000 kg)
|
|
gptkbp:wingspan
|
78 feet (24 m)
|
|
gptkbp:bfsParent
|
gptkb:Lockheed_Martin_Skunk_Works
|
|
gptkbp:bfsLayer
|
5
|