Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
0.35 m
|
| gptkbp:engine |
turbojet
|
| gptkbp:guidanceSystem |
active radar homing
inertial guidance |
| https://www.w3.org/2000/01/rdf-schema#label |
Exocet MM38
|
| gptkbp:introduced |
1975
|
| gptkbp:length |
5.08 m
|
| gptkbp:manufacturer |
gptkb:Aérospatiale
|
| gptkbp:partOf |
gptkb:Exocet_missile_family
|
| gptkbp:platform |
surface ship
|
| gptkbp:propulsion |
solid fuel rocket booster
|
| gptkbp:range |
42 km
|
| gptkbp:successor |
Exocet MM40
|
| gptkbp:usedBy |
gptkb:Royal_Navy
gptkb:French_Navy |
| gptkbp:usedInConflict |
gptkb:Falklands_War
|
| gptkbp:warheadType |
high-explosive fragmentation
165 kg |
| gptkbp:weight |
735 kg
|
| gptkbp:bfsParent |
gptkb:Exocet_MM40_missiles
gptkb:MM40 |
| gptkbp:bfsLayer |
6
|