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gptkbp:instance_of
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gptkb:Team_Rocket
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gptkbp:academic_programs
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comprised of experienced engineers
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gptkbp:collaboration
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involves international partners
NASA and Northrop Grumman
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gptkbp:configuration
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two-stage launch vehicle
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gptkbp:control_system
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digital flight control system
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gptkbp:debut
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multiple successful launches
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gptkbp:design_purpose
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to deliver cargo to the ISS
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gptkbp:designed_for
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commercial cargo resupply missions
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gptkbp:development_cost
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significant investment
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gptkbp:diameter
|
3.9 meters
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|
gptkbp:engine_type
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gptkb:Team_Rocket
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|
gptkbp:environmental_impact
|
designed to minimize environmental impact
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|
gptkbp:first_flight
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gptkb:2013
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gptkbp:fuel_type
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RP-1 and liquid oxygen
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|
gptkbp:future_plans
|
upgrades for increased payload capacity
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gptkbp:guidance_system
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gptkb:navigation_system
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|
gptkbp:has_limitations
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limited by payload size and weight
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|
gptkbp:has_tour
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uses a two-stage configuration
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gptkbp:height
|
approximately 14.5 meters
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Antares second stage
|
|
gptkbp:is_tested_for
|
extensive testing prior to launch
|
|
gptkbp:launch_date
|
multiple launches per year
|
|
gptkbp:launch_mass
|
approximately 20,000 kg
|
|
gptkbp:launch_platform
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gptkb:Northrop_Grumman_Innovation_Systems
|
|
gptkbp:launch_site
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gptkb:Wallops_Flight_Facility
|
|
gptkbp:launch_vehicle
|
configured for specific missions
part of Antares launch vehicle family
|
|
gptkbp:launched
|
gptkb:Mid-Atlantic_Regional_Spaceport
requires extensive launch preparation
|
|
gptkbp:manufacturer
|
gptkb:Northrop_Grumman
|
|
gptkbp:mission
|
high mission success rate
|
|
gptkbp:mission_duration
|
varies by mission
|
|
gptkbp:mission_type
|
orbital insertion
|
|
gptkbp:operated_by
|
gptkb:NASA
gptkb:RD-181_engines
|
|
gptkbp:operational_since
|
gptkb:2013
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|
gptkbp:operational_status
|
active
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gptkbp:part_of
|
gptkb:Antares_rocket
|
|
gptkbp:payload_capacity
|
up to 5,000 kg
optional payload fairing
capable of deploying multiple payloads
integrated with Cygnus spacecraft
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|
gptkbp:project
|
managed by Northrop Grumman
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|
gptkbp:propulsion
|
approximately 400 k N
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:safety_record
|
good safety record
|
|
gptkbp:successor
|
gptkb:Antares_230+
|
|
gptkbp:support
|
supports ISS resupply missions
|
|
gptkbp:technology
|
advanced aerospace technology
|
|
gptkbp:used_in
|
Cygnus spacecraft missions
|
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gptkbp:bfsParent
|
gptkb:Cygnus_CRS_OA-6
gptkb:Cygnus_CRS_OA-25
gptkb:Cygnus_CRS_OA-42
gptkb:Cygnus_CRS_OA-50
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gptkbp:bfsLayer
|
7
|