|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:air_traffic_control
|
fly-by-wire
|
|
gptkbp:block_upgrade
|
Block 5
Block 1
Block 2
Block 3
Block 4
|
|
gptkbp:block5_features
|
increased payload capacity
improved reusability
upgraded avionics
faster turnaround time
expanded fuel capacity
new grid fins
stronger landing legs
|
|
gptkbp:cargo_capacity
|
up to 6,000 kg to ISS
up to 22,800 kg to LEO
|
|
gptkbp:check_in_time
|
gptkb:1
6 minutes
multiple
2 minutes 30 seconds
approximately 162 seconds
approximately 397 seconds
|
|
gptkbp:collaboration
|
NASA, commercial customers
|
|
gptkbp:commercial_crew_program
|
gptkb:NASA
|
|
gptkbp:commercial_missions
|
gptkb:Starlink_satellites
|
|
gptkbp:commercial_use
|
yes
|
|
gptkbp:control_system
|
gptkb:navigation_system
|
|
gptkbp:crew
|
gptkb:Dragon
|
|
gptkbp:crew_capacity
|
gptkb:7
up to 7
up to 7 astronauts
7 astronauts
up to 4,000 kg of cargo
|
|
gptkbp:crew_transport
|
Crew Dragon missions
|
|
gptkbp:crew_transport_capability
|
yes
|
|
gptkbp:debut
|
June 4, 2010
extensive
over 150 launches
over a decade of service
|
|
gptkbp:designed_for
|
gptkb:Space_Launch_System
|
|
gptkbp:developed_by
|
gptkb:Space_X
|
|
gptkbp:development_cost
|
$300 million
approximately $500 million
|
|
gptkbp:diameter
|
3.7 meters
3.7 m
|
|
gptkbp:durability
|
gptkb:first_stage
gptkb:Yes
gptkb:true
yes
first stage can be reused multiple times
first stage can be reused up to 10 times
|
|
gptkbp:emergency_services
|
gptkb:GPS
gptkb:Dunmer
gptkb:Yes
yes
IMU
real-time data processing
accelerometer
control algorithms
autonomous guidance
autonomous drone ship
thrusters
drone ship
navigation sensors
landing legs
December 21, 2015
drone ship or ground pad
grid fins
land-based landing zone
land pad
flight termination system
|
|
gptkbp:engine
|
gptkb:Merlin
|
|
gptkbp:engine_type
|
gptkb:Merlin
gptkb:Team_Rocket
|
|
gptkbp:falcon_heavy
|
derived from Falcon 9
|
|
gptkbp:falcon9_block5
|
latest version
|
|
gptkbp:first_flight
|
gptkb:SES-10
gptkb:2010
gptkb:Falcon_9_Flight_1
June 4, 2010
ongoing
2010-06-04
|
|
gptkbp:first_reflight_date
|
March 30, 2017
|
|
gptkbp:first_reused_flight_date
|
March 30, 2017
|
|
gptkbp:first_stage_boostback
|
yes
|
|
gptkbp:first_stage_booster
|
gptkb:Falcon_9_Block_5
|
|
gptkbp:first_stage_booster_landing
|
autonomous drone ship
|
|
gptkbp:first_stage_booster_reuse_count
|
multiple
|
|
gptkbp:first_stage_burn_duration
|
2 minutes 30 seconds
approximately 2.5 minutes
|
|
gptkbp:first_stage_burns
|
gptkb:1
|
|
gptkbp:first_stage_diameter
|
3.7 m
|
|
gptkbp:first_stage_engine_thrust
|
845 k N
|
|
gptkbp:first_stage_engine_type
|
gptkb:Merlin_1_D
|
|
gptkbp:first_stage_flight_time
|
approximately 2.5 minutes
|
|
gptkbp:first_stage_fuel
|
RP-1 and Liquid Oxygen
|
|
gptkbp:first_stage_grid_fins
|
gptkb:4
|
|
gptkbp:first_stage_grid_fins_type
|
Active
|
|
gptkbp:first_stage_height
|
47.7 meters
47.7 m
|
|
gptkbp:first_stage_landing_accuracy
|
within 10 meters of target
|
|
gptkbp:first_stage_landing_attempts
|
over 100
|
|
gptkbp:first_stage_landing_failure
|
rare
|
|
gptkbp:first_stage_landing_legs
|
gptkb:4
|
|
gptkbp:first_stage_landing_legs_type
|
Retractable
|
|
gptkbp:first_stage_landing_location
|
gptkb:Cape_Canaveral
gptkb:ocean
gptkb:agricultural_land
Offshore drone ship
Onshore landing zone
|
|
gptkbp:first_stage_landing_speed
|
approximately 8 m/s
|
|
gptkbp:first_stage_landing_success
|
yes
|
|
gptkbp:first_stage_landing_success_rate
|
high
|
|
gptkbp:first_stage_landing_successes
|
over 80
|
|
gptkbp:first_stage_landing_type
|
autonomous drone ship
Landing on drone ship
ground pad
|
|
gptkbp:first_stage_landing_zone
|
LZ-1 or LZ-2
|
|
gptkbp:first_stage_landing_zone_location
|
gptkb:Cape_Canaveral
|
|
gptkbp:first_stage_recovery_attempts
|
Over 100
|
|
gptkbp:first_stage_recovery_location
|
gptkb:ocean
|
|
gptkbp:first_stage_recovery_success_rate
|
80%
|
|
gptkbp:first_stage_recovery_successes
|
Over 80
|
|
gptkbp:first_stage_recovery_type
|
vertical landing
|
|
gptkbp:first_stage_refurbishment
|
required after each flight
|
|
gptkbp:first_stage_reuse
|
gptkb:common
|
|
gptkbp:first_stage_thrust_to_weight_ratio
|
150:1
|
|
gptkbp:first_successful_launch_location
|
gptkb:Cape_Canaveral_Air_Force_Station
|
|
gptkbp:first_successful_launch_mission
|
gptkb:COTS_Demo_Flight_1
|
|
gptkbp:first_successful_launch_outcome
|
Successful
|
|
gptkbp:first_vertical_landing
|
December 21, 2015
|
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
RP-1 and liquid oxygen
|
|
gptkbp:government_use
|
yes
|
|
gptkbp:guidance_system
|
gptkb:GPS
|
|
gptkbp:healthcare
|
real-time data transmission
|
|
gptkbp:height
|
70 m
70 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Falcon 9
|
|
gptkbp:international_use
|
yes
|
|
gptkbp:is_a_reusable_rocket
|
gptkb:true
|
|
gptkbp:is_active_in
|
gptkb:true
|
|
gptkbp:is_part_of
|
gptkb:Falcon_rocket_family
|
|
gptkbp:landing_distance
|
gptkb:true
autonomous drone ship
drone ship
Autonomous drone ship
|
|
gptkbp:launch_control_center
|
gptkb:Space_X_Launch_Complex_39_A
gptkb:Space_X_Launch_Complex_40
|
|
gptkbp:launch_date
|
Monthly
high
June 4, 2010
2010-06-04
multiple per month
up to 48 launches per year
up to 48 per year
|
|
gptkbp:launch_mass
|
549,054 kg
|
|
gptkbp:launch_platform
|
gptkb:Cape_Canaveral_Launch_Complex
gptkb:Kennedy_Space_Center_Launch_Complex
gptkb:Space_X_Headquarters
gptkb:Space_X
gptkb:Space_X_Mission_Control
Vertical launch
vertical launch
commercial and government customers
Space X control center
|
|
gptkbp:launch_price
|
$62 million
approximately $62 million
around $62 million
|
|
gptkbp:launch_site
|
gptkb:Vandenberg_Space_Force_Base
gptkb:Kennedy_Space_Center
gptkb:Cape_Canaveral_Air_Force_Station
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launch_vehicle
|
gptkb:Space_Launch_Complex_40
gptkb:Falcon
gptkb:Launch_Complex_39_A
part of the Falcon family
|
|
gptkbp:launch_window
|
variable
varies by mission
|
|
gptkbp:launched
|
gptkb:2010
gptkb:2012
gptkb:2013
over 150
over 200
over 150 missions
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:mass
|
549,054 kg
|
|
gptkbp:mission_type
|
gptkb:uncrewed_missions
|
|
gptkbp:nasacertification
|
gptkb:true
|
|
gptkbp:notable_feature
|
high reliability
multiple launches per month
quick turnaround time
vertical landing capability
|
|
gptkbp:notable_launches
|
gptkb:NASA_Commercial_Crew_Program
gptkb:Crew-2
gptkb:Crew-1
gptkb:Transporter-1
over 180
CRS-20
|
|
gptkbp:notable_mission
|
gptkb:Crew_Dragon_Demo-2
gptkb:Commercial_Crew_Program
gptkb:CRS-2
gptkb:Crew_Dragon_Demo-1
gptkb:Demo-1
gptkb:SES-10
gptkb:Telstar_19_VANTAGE
gptkb:Starlink_4
gptkb:Starlink_10
gptkb:Starlink_11
gptkb:Starlink_12
gptkb:Starlink_13
gptkb:Starlink_14
gptkb:Starlink_15
gptkb:Starlink_16
gptkb:Starlink_17
gptkb:Starlink_18
gptkb:Starlink_19
gptkb:Starlink_20
gptkb:Starlink_21
gptkb:Starlink_22
gptkb:Starlink_23
gptkb:Starlink_24
gptkb:Starlink_25
gptkb:Starlink_26
gptkb:Starlink_27
gptkb:Starlink_28
gptkb:Starlink_29
gptkb:Starlink_30
gptkb:Starlink_31
gptkb:Starlink_32
gptkb:Starlink_33
gptkb:Starlink_34
gptkb:Starlink_35
gptkb:Starlink_36
gptkb:Starlink_37
gptkb:Starlink_38
gptkb:Starlink_39
gptkb:Starlink_40
gptkb:Starlink_41
gptkb:Starlink_42
gptkb:Starlink_43
gptkb:Starlink_44
gptkb:Starlink_45
gptkb:Starlink_46
gptkb:Starlink_47
gptkb:Starlink_48
gptkb:Starlink_49
gptkb:Starlink_5
gptkb:Starlink_50
gptkb:Starlink_6
gptkb:Starlink_7
gptkb:Starlink_8
gptkb:Starlink_9
gptkb:Demo-2
gptkb:CRS-1
gptkb:Starlink_missions
gptkb:Transporter-1
gptkb:Starlink_1
Starlink launches
In-Flight Abort Test
Transporter-4
Transporter missions
Transporting cargo to ISS
|
|
gptkbp:number_of_boosters
|
gptkb:9
|
|
gptkbp:number_of_engines
|
gptkb:9
|
|
gptkbp:number_of_stages
|
gptkb:Merlin_engines
gptkb:Merlin_Vacuum_engine
2
reusable
9 Merlin engines
1 Merlin Vacuum engine
7,607 k N
981 k N
1,020 k N
1,700 k N
reusable booster
|
|
gptkbp:number_of_successful_landings
|
over 100
|
|
gptkbp:operated_by
|
gptkb:Space_X
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:orbital_altitude
|
28,000 km/h
|
|
gptkbp:part_of
|
gptkb:NASA's_Commercial_Crew_Program
gptkb:NASA's_Commercial_Resupply_Services
|
|
gptkbp:payload_capacity
|
gptkb:Yes
22,800 kg
8,300 kg
5.2 meters
22,800 kg to LEO
13.1 meters
5.2 meters in diameter
8,300 kg to GTO
satellites, cargo, crew
payload fairing can be reused
up to 8,300 kg to GTO
fairing recovery
|
|
gptkbp:payload_capacity_to__gto
|
8,300 kg
|
|
gptkbp:payload_capacity_to__leo
|
22,800 kg
|
|
gptkbp:payload_capacity_to_geostationary_transfer_orbit
|
8,300 kg
|
|
gptkbp:payload_capacity_to_low_earth_orbit
|
22,800 kg
|
|
gptkbp:payload_fairing_recovery
|
gptkb:Yes
|
|
gptkbp:payload_fairing_weight
|
1,500 kg
|
|
gptkbp:payload_to_geostationary_transfer_orbit
|
8,300 kg
|
|
gptkbp:payload_to_low_earth_orbit
|
22,800 kg
|
|
gptkbp:primary_use
|
satellite deployment
|
|
gptkbp:propulsion
|
1.7 million pounds
1,700 k N
|
|
gptkbp:recovery_method
|
gptkb:true
no
yes
successful
Landing on drone ship
Grid fins
landing on drone ship
not currently recovered
successful recovery on land or sea
|
|
gptkbp:release_country
|
yes
|
|
gptkbp:reliability
|
high
|
|
gptkbp:reusability_count
|
up to 10 times
|
|
gptkbp:reuse_of_first_stage
|
up to 10 times
|
|
gptkbp:reused_first_stages
|
over 100
|
|
gptkbp:second_stage
|
single engine
not_reusable
|
|
gptkbp:second_stage_burn_duration
|
approximately 6 minutes
|
|
gptkbp:second_stage_diameter
|
3.7 m
|
|
gptkbp:second_stage_engine_thrust
|
981 k N
|
|
gptkbp:second_stage_engine_type
|
gptkb:Merlin_Vacuum
gptkb:Merlin_1_D_Vacuum
|
|
gptkbp:second_stage_flight_time
|
approximately 6 minutes
|
|
gptkbp:second_stage_fuel
|
RP-1 and Liquid Oxygen
|
|
gptkbp:second_stage_height
|
13.1 meters
13.1 m
|
|
gptkbp:second_stage_landing_success_rate
|
not applicable
|
|
gptkbp:second_stage_payload_fairing
|
gptkb:Yes
|
|
gptkbp:second_stage_recovery_method
|
not recovered
|
|
gptkbp:second_stage_thrust_to_weight_ratio
|
100:1
200:1
|
|
gptkbp:significant_event
|
first reflight of an orbital class rocket
first private spacecraft to reach the ISS
first private spacecraft to reach orbit
first crewed flight of a commercial spacecraft
|
|
gptkbp:stage_separation
|
gptkb:true
|
|
gptkbp:strategic_goals
|
gptkb:1
|
|
gptkbp:success
|
Over 150
over 100
|
|
gptkbp:success_rate
|
high
over 95%
over 90%
|
|
gptkbp:thrust_at_sea_level
|
1,700 k N
|
|
gptkbp:thrust_in_vacuum
|
1,900 k N
|
|
gptkbp:type
|
gptkb:Team_Rocket
Reusable launch vehicle
reusable rocket
|
|
gptkbp:bfsParent
|
gptkb:The_National_Aeronautics_and_Space_Administration
gptkb:Elon_Musk
gptkb:National_Aeronautics_and_Space_Administration
gptkb:NASA
gptkb:Team_Rocket
|
|
gptkbp:bfsLayer
|
3
|