|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:agent
|
NASA, Lockheed Martin, Northrop Grumman
|
|
gptkbp:avionics
|
Digital flight control system
|
|
gptkbp:budget
|
$20 billion
|
|
gptkbp:challenges
|
Thermal protection
Heavy-lift capability
|
|
gptkbp:community_engagement
|
gptkb:High
|
|
gptkbp:controls
|
Inertial navigation system
|
|
gptkbp:crew
|
4 astronauts
|
|
gptkbp:design
|
15 years
never completed
NASA engineers
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:developer
|
2004-2010
|
|
gptkbp:durability
|
Not reusable
|
|
gptkbp:ends_at
|
2025
|
|
gptkbp:engine
|
gptkb:F-1_B
5 engines
|
|
gptkbp:engine_type
|
gptkb:Rocketdyne_F-1
|
|
gptkbp:first_flight
|
gptkb:2010
planned but never launched
None conducted
|
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
|
|
gptkbp:guidance_system
|
GPS and inertial guidance
|
|
gptkbp:has_programs
|
gptkb:Constellation_program
|
|
gptkbp:height
|
106 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ares V
|
|
gptkbp:influenced_by
|
gptkb:International_Space_Station_program
gptkb:spacecraft
|
|
gptkbp:infrastructure
|
New launch pad
|
|
gptkbp:inspiration
|
gptkb:software
|
|
gptkbp:is_a_destination_for
|
gptkb:planet
|
|
gptkbp:is_designed_to
|
Deep space exploration
launch cargo missions
|
|
gptkbp:launch_date
|
gptkb:2015
1 per year
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
Heavy-lift launch vehicle
1,200,000 kg
|
|
gptkbp:launched
|
Open-ended
|
|
gptkbp:legacy
|
Influenced future launch vehicle designs
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:market
|
Estimated $1 billion
|
|
gptkbp:mission
|
Crewed lunar missions
|
|
gptkbp:mission_duration
|
gptkb:Artemis_program
30 days
|
|
gptkbp:number_of_stages
|
gptkb:Ares_I
gptkb:Ares_V_Upper_Stage
|
|
gptkbp:operational_area
|
None planned
|
|
gptkbp:operational_status
|
Not operational
|
|
gptkbp:part_of
|
gptkb:NASA's_human_spaceflight_program
gptkb:Ares_program
|
|
gptkbp:produced_by
|
Cancelled
|
|
gptkbp:propulsion
|
3,800,000 lbf
|
|
gptkbp:related_to
|
gptkb:Orion_spacecraft
|
|
gptkbp:safety_features
|
Not rated
|
|
gptkbp:seating_capacity
|
5 meters
18800 kg to LEO
188 tons to LEO
|
|
gptkbp:setting
|
Two-stage
|
|
gptkbp:successor
|
gptkb:software
|
|
gptkbp:targets
|
100,000 kg to LEO
|
|
gptkbp:technology
|
Advanced propulsion systems
|
|
gptkbp:user_reviews
|
Preliminary design review completed.
|
|
gptkbp:bfsParent
|
gptkb:NASA
|
|
gptkbp:bfsLayer
|
3
|