gptkbp:instance_of
|
gptkb:aircraft
|
gptkbp:avionics
|
Advanced avionics suite
|
gptkbp:budget
|
$30 billion
|
gptkbp:cancellation_reason
|
Budget constraints
|
gptkbp:challenges
|
Development delays
|
gptkbp:collaborations
|
Limited international collaboration
|
gptkbp:controls
|
Fly-by-wire system
|
gptkbp:crew
|
6 astronauts
|
gptkbp:design
|
Human spaceflight
Conceptual design phase
|
gptkbp:designed_by
|
gptkb:NASA
|
gptkbp:engine_type
|
gptkb:Rocketdyne_J-2_X
|
gptkbp:environmental_impact
|
Considered in design phase
|
gptkbp:first_flight
|
gptkb:2009
No test flights conducted
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
|
gptkbp:height
|
gptkb:100_meters
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ares I Launch Vehicle
|
gptkbp:influenced_by
|
Shuttle-derived designs
|
gptkbp:inspiration
|
gptkb:software
|
gptkbp:launch_date
|
2015 (originally planned)
Not applicable due to cancellation
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
gptkbp:launch_vehicle
|
500,000 kg
|
gptkbp:launched
|
Varies by mission
|
gptkbp:legacy
|
Influenced future launch vehicle designs
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
Various contractors
|
gptkbp:mission
|
Crewed missions to the Moon and Mars
|
gptkbp:number_of_stages
|
gptkb:rocket
Liquid-fueled upper stage
|
gptkbp:operational_area
|
Not applicable due to cancellation
|
gptkbp:part_of
|
gptkb:Constellation_program
|
gptkbp:produced_by
|
Cancelled
|
gptkbp:project
|
gptkb:NASA_Constellation_Program_Office
2004 to 2010
|
gptkbp:public_perception
|
Mixed due to cancellation
|
gptkbp:related_to
|
gptkb:spacecraft
|
gptkbp:reliability
|
Not achieved due to cancellation
|
gptkbp:safety_features
|
gptkb:aircraft
|
gptkbp:seating_capacity
|
25,000 kg to LEO
|
gptkbp:setting
|
Two-stage rocket
|
gptkbp:successor
|
gptkb:Orion_spacecraft
gptkb:Space_Launch_System_(SLS)
|
gptkbp:user_reviews
|
Preliminary design review completed
|
gptkbp:bfsParent
|
gptkb:Dr._Robert_D._Braun
|
gptkbp:bfsLayer
|
6
|