|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:control_system
|
autonomous landing system
|
|
gptkbp:crew_capacity
|
7 astronauts
|
|
gptkbp:debut
|
over 150 launches
|
|
gptkbp:design
|
two-stage rocket
|
|
gptkbp:development_cost
|
$300 million
|
|
gptkbp:diameter
|
3.7 meters
|
|
gptkbp:durability
|
gptkb:true
up to 10 times
|
|
gptkbp:emergency_services
|
drone ship
land pad
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:first_flight
|
2010-06-04
|
|
gptkbp:first_generation
|
gptkb:Falcon_Heavy
|
|
gptkbp:first_stage_boostback
|
yes
|
|
gptkbp:first_stage_landing_legs
|
four landing legs
|
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
|
|
gptkbp:height
|
70 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Space X's Falcon 9
|
|
gptkbp:launch_date
|
multiple launches per month
|
|
gptkbp:launch_platform
|
gptkb:NASA
gptkb:Space_X_Mission_Control
commercial customers
|
|
gptkbp:launch_price
|
$62 million
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:mass
|
549,054 kg
|
|
gptkbp:notable_launches
|
gptkb:Transporter-3
gptkb:CRS-2
gptkb:Crew_Dragon_Demo-1
gptkb:Starlink_4
gptkb:GPS_III_SV04
|
|
gptkbp:notable_mission
|
gptkb:Demo-2
gptkb:CRS-1
gptkb:Transporter-1
gptkb:Starlink_1
In-Flight Abort Test
|
|
gptkbp:number_of_stages
|
9 Merlin engines
1 Merlin Vacuum engine
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:payload_capacity
|
22,800 kg
5.2 meters
rideshare missions
dedicated missions
|
|
gptkbp:payload_capacity_to_geostationary_transfer_orbit
|
8,300 kg
|
|
gptkbp:propulsion
|
1,700 k N
|
|
gptkbp:recovery_method
|
no
yes
|
|
gptkbp:success_rate
|
over 95%
|
|
gptkbp:used_for
|
satellite launches
cargo resupply missions
crew missions
interplanetary missions
|
|
gptkbp:bfsParent
|
gptkb:North_American_X-15
|
|
gptkbp:bfsLayer
|
6
|