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gptkbp:instance_of
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gptkb:spacecraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Dragon_CRS-12
|
|
gptkbp:check_in_time
|
180 seconds
360 seconds
|
|
gptkbp:controls
|
Inertial navigation system
|
|
gptkbp:debut_year
|
Extensive launch history
|
|
gptkbp:diameter
|
3.7 meters
|
|
gptkbp:durability
|
gptkb:battle
|
|
gptkbp:engine
|
gptkb:Merlin_1_D
gptkb:9
Clustered configuration
|
|
gptkbp:engine_type
|
gptkb:rocket
|
|
gptkbp:first_flight
|
2015-12-21
|
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
|
|
gptkbp:future_plans
|
Continued use for missions
|
|
gptkbp:guidance_system
|
gptkb:GPS
|
|
gptkbp:height
|
70 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Falcon 9 v1.2
|
|
gptkbp:launch_date
|
gptkb:Regular
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
gptkb:Cape_Canaveral_Space_Force_Station
Automated and manual control
|
|
gptkbp:launch_vehicle
|
gptkb:Falcon_9
|
|
gptkbp:launched
|
gptkb:battle
Over 50
Several months
Varies by mission
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:market
|
$62 million
|
|
gptkbp:mission
|
gptkb:Crew_Dragon_Demo-1
gptkb:SES-10
gptkb:CRS-1
gptkb:Space_X_Mission_Control
Starlink launches
High success rate
Falcon Heavy Demo
|
|
gptkbp:number_of_stages
|
2
Reusable
Single Merlin Vacuum Engine
|
|
gptkbp:operational_status
|
Retired
|
|
gptkbp:produced_by
|
Operational
|
|
gptkbp:propulsion
|
75:1
1,700 k N
|
|
gptkbp:release_region
|
gptkb:battle
|
|
gptkbp:replaced_by
|
gptkb:Falcon_9_Block_5
|
|
gptkbp:research
|
gptkb:battle
|
|
gptkbp:restoration
|
Landing on drone ship
Landing on land
Drone ship or land recovery
|
|
gptkbp:seating_capacity
|
22,800 kg
8,300 kg
5.2 meters
Crewed and uncrewed missions
Space X facilities
Multiple payloads possible
|
|
gptkbp:succeeded_by
|
gptkb:High
|