gptkbp:instance_of
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gptkb:Space_Launch_System
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gptkbp:debut
|
gptkb:2013
2023-08-01
successful and partial failures
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gptkbp:design_purpose
|
commercial spaceflight
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gptkbp:development_cost
|
$1.9 billion
|
gptkbp:diameter
|
3.9 meters
|
gptkbp:elevation
|
140,000 kg
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gptkbp:engine_type
|
gptkb:Team_Rocket
|
gptkbp:first_flight
|
2013-04-21
|
gptkbp:first_stage_diameter
|
3.9 meters
|
gptkbp:first_stage_fuel
|
RP-1 and liquid oxygen
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gptkbp:first_stage_length
|
9.8 meters
|
gptkbp:has_programs
|
COTS (Commercial Orbital Transportation Services)
|
gptkbp:height
|
13.8 meters
|
https://www.w3.org/2000/01/rdf-schema#label
|
Antares launch system
|
gptkbp:last_successful_launch
|
2023-08-01
|
gptkbp:launch_date
|
approximately 1-2 per year
|
gptkbp:launch_platform
|
gptkb:NASA_Wallops_Flight_Facility
|
gptkbp:launch_site
|
gptkb:Mid-Atlantic_Regional_Spaceport
|
gptkbp:launch_vehicle
|
gptkb:advanced_propulsion_systems
modular design
two-stage
ongoing improvements
high reliability
publicly available
expendable launch vehicle
two-stage rocket
ISS resupply missions
Antares family
based on Antares 1
commercial off-the-shelf parts
|
gptkbp:launch_vehicle_design_life
|
15 years
|
gptkbp:launched
|
gptkb:15
|
gptkbp:manufacturer
|
gptkb:Northrop_Grumman
|
gptkbp:mass
|
approximately 140,000 kg
|
gptkbp:notable_mission
|
gptkb:Cygnus_resupply_missions
|
gptkbp:number_of_stages
|
gptkb:RD-181
gptkb:Castor_30_XL
2
1,800 k N
40 k N
|
gptkbp:operated_by
|
gptkb:Northrop_Grumman_Innovation_Systems
|
gptkbp:operational_since
|
gptkb:2013
|
gptkbp:operational_status
|
active
|
gptkbp:payload_capacity
|
gptkb:spacecraft
5 meters
up to 5,000 kg
performed at Wallops Flight Facility
|
gptkbp:primary_contractor
|
gptkb:Northrop_Grumman
|
gptkbp:primary_use
|
cargo resupply to ISS
|
gptkbp:reliability
|
high
|
gptkbp:second_stage_diameter
|
2.4 meters
|
gptkbp:second_stage_fuel
|
hydrazine
|
gptkbp:second_stage_length
|
3.5 meters
|
gptkbp:successor
|
gptkb:Vulcan_Centaur
|
gptkbp:total_failed_launches
|
gptkb:3
|
gptkbp:total_successful_launches
|
gptkb:12
|
gptkbp:bfsParent
|
gptkb:AR1_rocket_engine
gptkb:RD-181
|
gptkbp:bfsLayer
|
6
|