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gptkbp:instance_of
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gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
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gptkbp:bfsParent
|
gptkb:Orbital_ATK
|
|
gptkbp:construction_material
|
Composite materials
|
|
gptkbp:controls
|
Inertial navigation system
|
|
gptkbp:debut_year
|
3 launches from 2013 to 2014
Comprehensive pre-launch checks
|
|
gptkbp:design
|
15 years
|
|
gptkbp:developer
|
gptkb:2008
$200 million
|
|
gptkbp:diameter
|
2.4 meters
|
|
gptkbp:elevation
|
120,000 kg
|
|
gptkbp:engine
|
gptkb:musical
gptkb:Aerojet_Rocketdyne
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:first_flight
|
2013-04-20
2014-01-09
|
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
|
|
gptkbp:guidance_system
|
GPS-based guidance
|
|
gptkbp:healthcare
|
Real-time telemetry
|
|
gptkbp:height
|
23.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Taurus II
|
|
gptkbp:launch_site
|
gptkb:Orbital_Sciences_Corporation
gptkb:Mid-Atlantic_Regional_Spaceport
gptkb:railway_station
Post-launch telemetry analysis
|
|
gptkbp:launch_vehicle
|
gptkb:Mid-Atlantic_Regional_Spaceport_Launch_Complex_0_A
gptkb:automobile
120,000 kg
Expendable launch vehicle
Two-stage configuration
|
|
gptkbp:launched
|
gptkb:Launch_Complex_0_A
gptkb:3
varies by mission
|
|
gptkbp:manufacturer
|
gptkb:Orbital_ATK
|
|
gptkbp:mission
|
commercial and government missions
Cygnus CRSOA-1
Orbital Sciences mission control
|
|
gptkbp:number_of_stages
|
gptkb:Castor_30
2
Orbus 21
|
|
gptkbp:operational_area
|
2013-2014
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:production_location
|
gptkb:Dulles,_Virginia
|
|
gptkbp:production_years
|
gptkb:2013
|
|
gptkbp:propulsion
|
300 k N
|
|
gptkbp:purpose
|
launching payloads into orbit
|
|
gptkbp:reliability
|
high
|
|
gptkbp:replaced_by
|
gptkb:Antares
|
|
gptkbp:seating_capacity
|
10 meters
Low Earth Orbit
5,000 kg
Vertical integration
2.5 meters in diameter
5,000 kg to LEO
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Antares
|
|
gptkbp:transportation
|
Rollout to launch pad
|