|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:avionics
|
Digital flight control system
|
|
gptkbp:budget
|
$20 billion
|
|
gptkbp:challenges
|
Thermal protection
Heavy-lift capability
|
|
gptkbp:configuration
|
Two-stage
|
|
gptkbp:control_system
|
Inertial navigation system
|
|
gptkbp:crew_capacity
|
4 astronauts
|
|
gptkbp:design
|
15 years
never completed
NASA engineers
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:development
|
2004-2010
|
|
gptkbp:durability
|
Not reusable
|
|
gptkbp:engine
|
gptkb:F-1_B
|
|
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:Space_Shuttle
|
|
gptkbp:infrastructure
|
New launch pad
|
|
gptkbp:inspiration
|
gptkb:Apollo_program
|
|
gptkbp:intended_use
|
Deep space exploration
|
|
gptkbp:is_a_destination_for
|
gptkb:Moon
|
|
gptkbp:is_designed_to
|
launch cargo missions
|
|
gptkbp:launch_date
|
gptkb:2015
|
|
gptkbp:launch_mass
|
1,200,000 kg
|
|
gptkbp:launch_price
|
Estimated $1 billion
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
Heavy-lift launch vehicle
|
|
gptkbp:launch_window
|
Open-ended
|
|
gptkbp:legacy
|
Influenced future launch vehicle designs
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:mission
|
Crewed lunar missions
|
|
gptkbp:mission_duration
|
30 days
|
|
gptkbp:number_of_engines
|
5 engines
|
|
gptkbp:number_of_stages
|
gptkb:Ares_I
gptkb:Ares_V_Upper_Stage
|
|
gptkbp:operational_status
|
Not operational
|
|
gptkbp:operational_use
|
None planned
|
|
gptkbp:parent_agency
|
NASA, Lockheed Martin, Northrop Grumman
|
|
gptkbp:part_of
|
gptkb:NASA's_human_spaceflight_program
gptkb:Ares_program
|
|
gptkbp:payload_capacity
|
5 meters
18800 kg to LEO
188 tons to LEO
|
|
gptkbp:production_status
|
Cancelled
|
|
gptkbp:projected_crewed_missions
|
gptkb:Artemis_program
|
|
gptkbp:projected_end_of_service
|
2025
|
|
gptkbp:projected_launch_frequency
|
1 per year
|
|
gptkbp:projected_payload
|
100,000 kg to LEO
|
|
gptkbp:projected_technology
|
Advanced propulsion systems
|
|
gptkbp:propulsion
|
3,800,000 lbf
|
|
gptkbp:public_interest
|
gptkb:High
|
|
gptkbp:related_to
|
gptkb:Orion_spacecraft
|
|
gptkbp:reviews
|
Preliminary design review completed.
|
|
gptkbp:safety_rating
|
Not rated
|
|
gptkbp:successor
|
gptkb:Space_Launch_System
|
|
gptkbp:bfsParent
|
gptkb:NASA
|
|
gptkbp:bfsLayer
|
3
|