Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:firstFlight |
1956
|
| gptkbp:guidanceSystem |
inertial guidance
|
| https://www.w3.org/2000/01/rdf-schema#label |
Regulus II
|
| gptkbp:length |
17.7 m
|
| gptkbp:manufacturer |
gptkb:Hughes_Aircraft
|
| gptkbp:platform |
gptkb:marine
surface ship |
| gptkbp:predecessor |
gptkb:Regulus_I
|
| gptkbp:projectCancelled |
1958
|
| gptkbp:propulsion |
turbojet
|
| gptkbp:range |
1850 km
|
| gptkbp:speed |
Mach 2
|
| gptkbp:status |
canceled
|
| gptkbp:successor |
gptkb:Polaris_missile
|
| gptkbp:type |
gptkb:surface-to-air_missile
|
| gptkbp:usedBy |
gptkb:United_States_Navy
|
| gptkbp:warheadType |
nuclear
|
| gptkbp:wingspan |
6.4 m
|
| gptkbp:bfsParent |
gptkb:Regulus_cruise_missile
gptkb:Regulus_cruise_missiles |
| gptkbp:bfsLayer |
8
|