|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:The_Razor_Crest
gptkb:Starship_Razor_Crest
|
|
gptkbp:challenges
|
thermal protection system
|
|
gptkbp:construction_cost
|
$10 million
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:crew
|
gptkb:none
2
|
|
gptkbp:design
|
reusability
single-stage to orbit
|
|
gptkbp:designed_by
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:developer
|
$1 billion
NASA and Boeing
|
|
gptkbp:engine_type
|
gptkb:rocket
|
|
gptkbp:environmental_impact
|
reduced emissions
|
|
gptkbp:features
|
delta wing
|
|
gptkbp:first_flight
|
gptkb:1994
gptkb:1998
gptkb:1999
suborbital to orbital
12 flights per year
|
|
gptkbp:fuel_type
|
liquid hydrogen
|
|
gptkbp:goal
|
reduce launch costs
|
|
gptkbp:has_programs
|
Venture Star program
|
|
gptkbp:height
|
approximately 80 feet
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Venture Star
|
|
gptkbp:influenced_by
|
NASA's X-33
|
|
gptkbp:innovation
|
new propulsion technologies
|
|
gptkbp:inspiration
|
gptkb:X-15_program
|
|
gptkbp:investment
|
high
|
|
gptkbp:launch_date
|
gptkb:2001
bi-monthly
|
|
gptkbp:launch_site
|
gptkb:cape
gptkb:Kennedy_Space_Center
vertical launch
|
|
gptkbp:launch_vehicle
|
not applicable
approximately 100,000 pounds
|
|
gptkbp:manufacturer
|
gptkb:aircraft
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:market
|
commercial satellite launches
Space X and others
|
|
gptkbp:mission_duration
|
orbital insertion
|
|
gptkbp:operational_area
|
1990s to early 2000s
not achieved
$5 million per flight
|
|
gptkbp:partnerships
|
aerospace companies
|
|
gptkbp:performance
|
low Earth orbit missions
|
|
gptkbp:primary_user
|
government and commercial sectors
|
|
gptkbp:project
|
gptkb:patent
|
|
gptkbp:purpose
|
reusable launch vehicle
to transport payloads to low Earth orbit
|
|
gptkbp:receives_funding_from
|
government and private investment
|
|
gptkbp:regulatory_compliance
|
FAA regulations
|
|
gptkbp:related_to
|
gptkb:spacecraft
|
|
gptkbp:safety_record
|
high safety standards
|
|
gptkbp:seating_capacity
|
15,000 pounds to LEO
|
|
gptkbp:service_years
|
10 years
|
|
gptkbp:status
|
canceled
|
|
gptkbp:successor
|
gptkb:X-33
|
|
gptkbp:target_audience
|
high
|
|
gptkbp:target_market
|
space tourism and research.
|
|
gptkbp:targets
|
20,000 pounds to LEO
|
|
gptkbp:technology
|
advanced composite materials
single-stage-to-orbit
reusable systems
|
|
gptkbp:ticket_sales
|
customizable
|
|
gptkbp:type
|
reusable launch vehicle
|
|
gptkbp:weight
|
approximately 100,000 pounds
|
|
gptkbp:wingspan
|
approximately 70 feet
|