Statements (14)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:cancellationDate |
1942
|
| gptkbp:countryOfOrigin |
gptkb:Germany
|
| gptkbp:designer |
Adolf Müller
|
| gptkbp:developedBy |
gptkb:World_War_II
|
| gptkbp:engineType |
axial-flow turbojet
|
| gptkbp:firstFlight |
1941
|
| https://www.w3.org/2000/01/rdf-schema#label |
Heinkel HeS 30
|
| gptkbp:intendedUse |
aircraft propulsion
|
| gptkbp:manufacturer |
gptkb:Heinkel
|
| gptkbp:status |
gptkb:prototype
|
| gptkbp:thrust |
860 kgf
|
| gptkbp:bfsParent |
gptkb:Heinkel_HeS_8
|
| gptkbp:bfsLayer |
8
|