|
gptkbp:instanceOf
|
rocket stage
|
|
gptkbp:annualRidership
|
over 100
|
|
gptkbp:chemicalFormula
|
liquid oxygen
|
|
gptkbp:controls
|
grid fins
|
|
gptkbp:design
|
approximately 2 years
two-stage rocket
|
|
gptkbp:developer
|
ongoing improvements
|
|
gptkbp:diameter
|
3.7 meters
|
|
gptkbp:engine
|
gptkb:Merlin_1D
|
|
gptkbp:engineConfiguration
|
single engine
|
|
gptkbp:firstFlight
|
2010-06-04
|
|
gptkbp:fuelType
|
kerosene
|
|
gptkbp:gameFeatures
|
RP-1
liquid oxygen
|
|
gptkbp:height
|
4.6 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Falcon 9 second stage
|
|
gptkbp:landingGear
|
not designed for landing
|
|
gptkbp:launchDate
|
frequent
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:manufacturer
|
gptkb:SpaceX
|
|
gptkbp:mission
|
deliver payloads to orbit
|
|
gptkbp:missions
|
gptkb:Starlink
Crew Dragon
Transporter missions
|
|
gptkbp:number_of_stages
|
approximately 2 minutes after launch
|
|
gptkbp:operational_status
|
active
scientific missions
commercial launches
government missions
|
|
gptkbp:operationalHistory
|
2010
|
|
gptkbp:passenger_traffic
|
optional
4,000 kg
8,300 kg
|
|
gptkbp:propulsion
|
934 kN
> 100:1
|
|
gptkbp:provides
|
inertial navigation
|
|
gptkbp:related_engine
|
gas-generator cycle
|
|
gptkbp:reliability
|
yes
high
|
|
gptkbp:succeededBy
|
over 95%
|
|
gptkbp:tourism
|
approximately 6 minutes
|
|
gptkbp:uses
|
for ISS resupply missions
for interplanetary missions
for satellite deployment
|