Falcon 9 second stage (MVac)
GPTKB entity
Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
3.66 m
|
| gptkbp:engine |
gptkb:Merlin_1D_Vacuum
|
| gptkbp:engineType |
gptkb:Merlin_Vacuum_(MVac)
|
| gptkbp:firstFlight |
2010-06-04
|
| gptkbp:fuelType |
gptkb:RP-1
|
| gptkbp:guidanceSystem |
autonomous
|
| https://www.w3.org/2000/01/rdf-schema#label |
Falcon 9 second stage (MVac)
|
| gptkbp:ignitionCapability |
multiple restart
|
| gptkbp:length |
12.6 m
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:material |
aluminum-lithium alloy
|
| gptkbp:minimumPressure |
autogenous
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:RP-1
liquid oxygen |
| gptkbp:reusable |
expendable
|
| gptkbp:status |
active
|
| gptkbp:thrustVacuum |
981 kN
|
| gptkbp:usedFor |
orbital insertion
payload deployment |
| gptkbp:usedOn |
gptkb:Falcon_9_v1.0
gptkb:Falcon_9 gptkb:Falcon_9_Block_4 gptkb:Falcon_9_Block_5 gptkb:Falcon_9_v1.1 |
| gptkbp:bfsParent |
gptkb:SpaceX_Merlin
|
| gptkbp:bfsLayer |
6
|