gptkbp:instance_of
|
gptkb:Team_Rocket
|
gptkbp:avionics
|
advanced
|
gptkbp:budget
|
$30 billion
|
gptkbp:challenges
|
aerodynamics
complex systems integration
|
gptkbp:collaboration
|
possible
|
gptkbp:control_system
|
Fly-by-wire
|
gptkbp:crew
|
required
|
gptkbp:crew_capacity
|
gptkb:6
|
gptkbp:decided_by
|
cancellation in 2010
|
gptkbp:design
|
10 years
completed
|
gptkbp:designed_by
|
gptkb:NASA
|
gptkbp:development
|
gptkb:2004
|
gptkbp:diameter
|
5.2 meters
|
gptkbp:engine_type
|
gptkb:liquid
|
gptkbp:environmental_impact
|
assessed
|
gptkbp:first_flight
|
gptkb:2009
gptkb:Ares_I-X
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
|
gptkbp:guidance_system
|
inertial navigation
|
gptkbp:has_programs
|
gptkb:Constellation_program
|
gptkbp:height
|
98 meters
|
https://www.w3.org/2000/01/rdf-schema#label
|
NASA's Ares I rocket
|
gptkbp:influenced
|
gptkb:Space_Launch_System_(SLS)
|
gptkbp:inspiration
|
gptkb:Apollo_program
|
gptkbp:involved_in
|
Lunar missions
|
gptkbp:launch_date
|
gptkb:2015
annual
|
gptkbp:launch_mass
|
500,000 kg
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
gptkbp:launch_vehicle
|
gptkb:Ares_I-X
|
gptkbp:launch_window
|
2010s
|
gptkbp:legacy
|
influenced future rockets
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
gptkbp:mission_duration
|
up to 30 days
|
gptkbp:mission_type
|
gptkb:exploration
|
gptkbp:number_of_stages
|
gptkb:J-2_X_engine
gptkb:Team_Rocket
|
gptkbp:operational_cost
|
estimated $1 billion per launch
|
gptkbp:orbital_altitude
|
7.8 km/s
|
gptkbp:payload_capacity
|
25,000 kg
|
gptkbp:production_years
|
gptkb:2010
|
gptkbp:propulsion
|
1,000,000 lbf
|
gptkbp:public_interest
|
high
|
gptkbp:purpose
|
gptkb:human_spaceflight
|
gptkbp:related_to
|
gptkb:Artemis_program
|
gptkbp:reliability
|
high
|
gptkbp:safety_features
|
redundant systems
|
gptkbp:status
|
canceled
|
gptkbp:successor
|
gptkb:Orion_spacecraft
|
gptkbp:bfsParent
|
gptkb:NASA's_Marshall_Space_Flight_Center
|
gptkbp:bfsLayer
|
5
|