Statements (54)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft
|
| gptkbp:aircraft |
200 km
|
| gptkbp:aspectRatio |
20:1
|
| gptkbp:barrelLength |
2 degrees/second
|
| gptkbp:category |
experimental aircraft
|
| gptkbp:cockpit |
open cockpit
glider pilot license |
| gptkbp:constructionMaterial |
monocoque
high-performance airfoil |
| gptkbp:controls |
ailerons
elevator rudder stick and rudder |
| gptkbp:countryOfOrigin |
gptkb:Germany
|
| gptkbp:currentStatus |
not in production
preserved in a museum |
| gptkbp:design |
research and development
winglets retractable landing gear high lift devices |
| gptkbp:designedBy |
Klaus_Kremer
|
| gptkbp:engineType |
none
|
| gptkbp:firstFlight |
1984
|
| gptkbp:flag |
2 degrees/second
|
| gptkbp:headlights |
T-tail
|
| https://www.w3.org/2000/01/rdf-schema#label |
Kremer K4
|
| gptkbp:landingGear |
fixed gear
|
| gptkbp:length |
8.5 meters
|
| gptkbp:maintenance |
low maintenance requirements
|
| gptkbp:material |
composite materials
|
| gptkbp:maximumDepth |
3000 meters
|
| gptkbp:maxSpeed |
120 km/h
|
| gptkbp:missions |
manual
|
| gptkbp:numberOfSeasons |
1
|
| gptkbp:operationalHistory |
used for training purposes
retired from active service used in various competitions participated in airshows flown by experienced pilots |
| gptkbp:performance |
high maneuverability
responsive handling stable flight characteristics low stall speed excellent glide ratio |
| gptkbp:productionYears |
1984
|
| gptkbp:safetyFeatures |
parachute system
crash-resistant cockpit |
| gptkbp:speed |
60 km/h
|
| gptkbp:succeededBy |
3 degrees/second
|
| gptkbp:type |
glider
|
| gptkbp:usedFor |
gliding competitions
|
| gptkbp:weight |
300 kg
|
| gptkbp:wingArea |
15 m²
|
| gptkbp:wingspan |
15.5 meters
|