|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:RD-181
|
|
gptkbp:debut_year
|
gptkb:2013
2023-08-01
successful and partial failures
|
|
gptkbp:design
|
commercial spaceflight
|
|
gptkbp:developer
|
$1.9 billion
|
|
gptkbp:diameter
|
2.4 meters
3.9 meters
|
|
gptkbp:elevation
|
140,000 kg
|
|
gptkbp:engine_type
|
gptkb:rocket
|
|
gptkbp:first_flight
|
2013-04-21
|
|
gptkbp:fuel_type
|
hydrazine
RP-1 and liquid oxygen
|
|
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:launch_date
|
2023-08-01
approximately 1-2 per year
|
|
gptkbp:launch_site
|
gptkb:NASA_Wallops_Flight_Facility
gptkb:Mid-Atlantic_Regional_Spaceport
|
|
gptkbp:launch_vehicle
|
gptkb:advanced_propulsion_systems
15 years
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:launched
|
gptkb:12
gptkb:15
gptkb:3
|
|
gptkbp:manufacturer
|
gptkb:Northrop_Grumman
|
|
gptkbp:mass
|
approximately 140,000 kg
|
|
gptkbp:mission
|
gptkb:Cygnus_resupply_missions
|
|
gptkbp:number_of_stages
|
gptkb:RD-181
gptkb:Castor_30_XL
2
3.5 meters
9.8 meters
1,800 k N
40 k N
|
|
gptkbp:operated_by
|
gptkb:Northrop_Grumman_Innovation_Systems
|
|
gptkbp:operational_status
|
gptkb:2013
active
|
|
gptkbp:primary_source
|
cargo resupply to ISS
|
|
gptkbp:primary_user
|
gptkb:Northrop_Grumman
|
|
gptkbp:reliability
|
high
|
|
gptkbp:seating_capacity
|
gptkb:spacecraft
5 meters
up to 5,000 kg
performed at Wallops Flight Facility
|
|
gptkbp:successor
|
gptkb:Vulcan_Centaur
|