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gptkbp:instance_of
|
gptkb:Author
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Lunar_Module_Antares
|
|
gptkbp:controls
|
digital flight control system
|
|
gptkbp:debut_year
|
August 2021
October 28, 2013
|
|
gptkbp:designed_by
|
gptkb:Northrop_Grumman
|
|
gptkbp:developer
|
$200 million
|
|
gptkbp:diameter
|
3.9 meters
|
|
gptkbp:engine_type
|
gptkb:RD-181
|
|
gptkbp:first_flight
|
gptkb:2013
|
|
gptkbp:fuel_type
|
RP-1 and liquid oxygen
|
|
gptkbp:guidance_system
|
gptkb:hospital
|
|
gptkbp:height
|
approximately 14 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Antares descent stage
|
|
gptkbp:launch_date
|
approximately 2-3 times per year
|
|
gptkbp:launch_site
|
gptkb:Northrop_Grumman
gptkb:Wallops_Flight_Facility
|
|
gptkbp:launch_vehicle
|
gptkb:Antares_230+
|
|
gptkbp:launched
|
gptkb:Mid-Atlantic_Regional_Spaceport
|
|
gptkbp:manufacturer
|
gptkb:Northrop_Grumman_Innovation_Systems
|
|
gptkbp:mission
|
cargo resupply
|
|
gptkbp:mission_duration
|
approximately 30 days
|
|
gptkbp:operational_status
|
gptkb:2013
active
|
|
gptkbp:part_of
|
gptkb:Antares_rocket
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:replaced_by
|
gptkb:Antares_130
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:seating_capacity
|
up to 3,500 kg
5-meter diameter
|
|
gptkbp:setting
|
two-stage rocket
|
|
gptkbp:succeeded_by
|
over 90%
|
|
gptkbp:supports
|
gptkb:International_Space_Station
|
|
gptkbp:used_in
|
gptkb:spacecraft
|