Properties (58)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
Launch Vehicle
|
| gptkbp:capacity |
22,800 kg to LEO
|
| gptkbp:country |
gptkb:United_States
|
| gptkbp:design |
Two-stage rocket
|
| gptkbp:developer |
$500 million
|
| gptkbp:diameter |
3.7 m
|
| gptkbp:engine |
9
1,700 kN per engine |
| gptkbp:engineConfiguration |
gptkb:Octaweb
|
| gptkbp:engineType |
gptkb:Merlin
High performance RP-1/LOX Merlin_engine_ignition |
| gptkbp:firstAwarded |
9
Yes On land or drone ship |
| gptkbp:firstFlight |
Yes
2020-05-30 |
| gptkbp:height |
70 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
LC-1
|
| gptkbp:IATA_code |
Numerous successful missions
|
| gptkbp:launchDate |
Multiple successful launches
|
| gptkbp:launched |
gptkb:SpaceX
$62 million Flexible Frequent Ground support equipment SpaceX_control_center |
| gptkbp:launchSite |
gptkb:Cape_Canaveral_Space_Force_Station
|
| gptkbp:launchVehicle |
gptkb:Falcon
Regular updates and improvements Expendable Detailed specifications available Advanced features for reliability Commercial and government applications Reusable design Standard configuration Variants available for different missions Part_of_the_Falcon_family_history |
| gptkbp:manufacturer |
gptkb:United_States
gptkb:SpaceX |
| gptkbp:mission |
Satellite_Launch
|
| gptkbp:missionCapabilities |
Low Earth Orbit
|
| gptkbp:missionsConducted |
High
|
| gptkbp:number_of_stages |
2
|
| gptkbp:operationalStatus |
Operational
|
| gptkbp:orbitalInclination |
51.6 degrees
|
| gptkbp:passenger_traffic |
22,800 kg
5.2 m In orbit Crewed and uncrewed missions Integrated at SpaceX facilities |
| gptkbp:payloadCapacity |
8,300 kg to GTO
|
| gptkbp:propulsion |
7,607 kN
|
| gptkbp:releaseFormat |
LC-39A
|
| gptkbp:reliability |
Yes
|
| gptkbp:renovated |
Yes
|
| gptkbp:status |
Active
|