Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:alsoKnownAs |
gptkb:aircraft
|
| gptkbp:application |
ground ramp
aircraft launch |
| gptkbp:countryOfOrigin |
gptkb:Nazi_Germany
|
| gptkbp:designedBy |
gptkb:Robert_Lusser
|
| gptkbp:enteredService |
1944
|
| gptkbp:firstFlight |
1942
|
| gptkbp:guidanceSystem |
gyroscopic autopilot
|
| https://www.w3.org/2000/01/rdf-schema#label |
Fieseler Fi 103E
|
| gptkbp:length |
8.32 m
|
| gptkbp:manufacturer |
gptkb:Fieseler
|
| gptkbp:primaryUser |
Luftwaffe
|
| gptkbp:propulsion |
piston engine
|
| gptkbp:range |
250 km
|
| gptkbp:speed |
640 km/h
|
| gptkbp:status |
retired
|
| gptkbp:usedInConflict |
gptkb:World_War_II
|
| gptkbp:warheadType |
850 kg
|
| gptkbp:wingspan |
5.37 m
|
| gptkbp:bfsParent |
gptkb:Gerhard_Fieseler_Werke
|
| gptkbp:bfsLayer |
6
|