Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:armament |
gptkb:2×_30_mm_DEFA_cannons
external hardpoints for bombs and rockets |
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:crew |
1
|
| gptkbp:designedFor |
NATO Lightweight Strike Fighter competition
|
| gptkbp:emptyWeight |
5,000 kg
|
| gptkbp:engineType |
SNECMA Atar 101F turbojet
|
| gptkbp:firstFlight |
15 March 1957
|
| gptkbp:height |
3.75 m
|
| gptkbp:length |
13.15 m
|
| gptkbp:manufacturer |
gptkb:Dassault_Aviation
|
| gptkbp:maximumSpeed |
1,120 km/h
|
| gptkbp:maxTakeoffWeight |
8,500 kg
|
| gptkbp:notableFor |
did not enter production
|
| gptkbp:numberBuilt |
2
|
| gptkbp:role |
gptkb:aircraft
fighter |
| gptkbp:status |
gptkb:prototype
|
| gptkbp:successor |
gptkb:Dassault_Étendard_IV
|
| gptkbp:usedIn |
NATO competition
|
| gptkbp:wingspan |
8.60 m
|
| gptkbp:bfsParent |
gptkb:Dassault_Étendard
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Dassault Étendard VI
|