|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:air_traffic_control
|
digital flight control system
|
|
gptkbp:avionics
|
advanced avionics system
|
|
gptkbp:control_system
|
fly-by-wire
|
|
gptkbp:crew_capacity
|
2
|
|
gptkbp:debut_year
|
gptkb:1996
gptkb:2001
|
|
gptkbp:design
|
gptkb:prototype
|
|
gptkbp:design_purpose
|
reduce launch costs
|
|
gptkbp:designed_by
|
gptkb:Lockheed_Martin
|
|
gptkbp:durability
|
high
|
|
gptkbp:elevation
|
100 km
|
|
gptkbp:endurance
|
1 hour
|
|
gptkbp:engine_type
|
linear aerospike engine
|
|
gptkbp:first_flight
|
gptkb:1999
2
mixed results
March 1999
|
|
gptkbp:fuel_type
|
liquid hydrogen
|
|
gptkbp:fuselage_material
|
composite materials
|
|
gptkbp:has_a_focus_on
|
vertical takeoff and landing
|
|
gptkbp:has_programs
|
gptkb:X-33_program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
X-33 Venture Star
|
|
gptkbp:influenced_by
|
gptkb:X-15_program
|
|
gptkbp:inspiration
|
gptkb:Space_Shuttle
|
|
gptkbp:involved_technology
|
yes
advanced materials, aerodynamics
|
|
gptkbp:landing_gear
|
retractable
|
|
gptkbp:launch_mass
|
approximately 20,000 kg
|
|
gptkbp:launch_price
|
$10 million
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:monoplane
|
|
gptkbp:length
|
25.6 m
|
|
gptkbp:max_speed
|
Mach 15
|
|
gptkbp:mission_duration
|
up to 2 weeks
|
|
gptkbp:operational_status
|
not operational
|
|
gptkbp:operational_use
|
single-stage to orbit
|
|
gptkbp:parent_agency
|
NASA, Lockheed Martin
|
|
gptkbp:payload_capacity
|
15,000 kg
|
|
gptkbp:primary_contractor
|
gptkb:NASA
|
|
gptkbp:project
|
X-34, X-37
|
|
gptkbp:projected_crew_training
|
minimal
|
|
gptkbp:projected_launch_frequency
|
monthly
|
|
gptkbp:projected_mission_profile
|
suborbital and orbital missions
|
|
gptkbp:projected_operational_year
|
gptkb:2005
|
|
gptkbp:projected_payload_fairing
|
gptkb:none
|
|
gptkbp:purpose
|
reusable launch vehicle
|
|
gptkbp:range
|
low Earth orbit
|
|
gptkbp:status
|
canceled
|
|
gptkbp:successor
|
gptkb:Space_Launch_System
|
|
gptkbp:weight
|
approximately 20,000 kg
|
|
gptkbp:wingspan
|
23.5 m
|
|
gptkbp:bfsParent
|
gptkb:Lockheed_Martin_Skunk_Works
|
|
gptkbp:bfsLayer
|
5
|