Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
rocket engine family
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
gas-generator
|
| gptkbp:developedBy |
gptkb:SpaceX
|
| gptkbp:firstFlight |
2006
|
| gptkbp:fuelType |
gptkb:RP-1
|
| gptkbp:gimbalRange |
up to 15 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
Merlin engine family
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:notableFeature |
high reliability
throttleable ablatively cooled (early versions) designed for rapid manufacturing regeneratively cooled used in booster landings |
| gptkbp:notableMember |
gptkb:Merlin_1D
gptkb:Merlin_1A gptkb:Merlin_1B gptkb:Merlin_1C |
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:primaryUse |
first stage engines
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:reusable |
designed for reuse
|
| gptkbp:status |
active
|
| gptkbp:thrust |
400 kN to 845 kN
|
| gptkbp:usedFor |
orbital launch vehicles
|
| gptkbp:usedIn |
gptkb:Falcon_1
gptkb:Falcon_9 gptkb:Falcon_Heavy |
| gptkbp:bfsParent |
gptkb:Merlin_100
|
| gptkbp:bfsLayer |
7
|