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- HKS-1 abstract "The HKS-1 was a German 19 span high performance two seat sailplane, designed around 1950 to use recent advances in laminar flow airfoils. To avoid premature transition from laminar flow caused by surface interruptions, the HKS-1 dispensed with hinged ailerons, flaps and spoilers and replaced them with a flexible trailing edge. Two were built, setting several records.".
- HKS-1 manufacturer Haase-Kensche-Schmetz.
- HKS-1 numberBuilt "2".
- HKS-1 origin Germany.
- HKS-1 type Glider_(sailplane).
- HKS-1 wikiPageID "34859805".
- HKS-1 wikiPageRevisionID "592001873".
- HKS-1 airfoil "NACA 65215-714".
- HKS-1 aspectRatio "20.3".
- HKS-1 crew "2".
- HKS-1 designer "Ernst Gúnther Haase, Heinz Kensche and Fernando Schmetz".
- HKS-1 developedInto HKS-3.
- HKS-1 emptyWeightKg "440".
- HKS-1 emptyWeightNote "equipped".
- HKS-1 firstFlight "July 1953".
- HKS-1 gLimits "2".
- HKS-1 glideRatio "37.2".
- HKS-1 hasPhotoCollection HKS-1.
- HKS-1 lengthM "8.25".
- HKS-1 lists "* List of gliders".
- HKS-1 manufacturer Haase-Kensche-Schmetz.
- HKS-1 maxTakeoffWeightKg "620".
- HKS-1 minimumControlSpeedKmh "70".
- HKS-1 nationalOrigin Germany.
- HKS-1 neverExceedSpeedKmh "230".
- HKS-1 neverExceedSpeedNote "*Rough air speed max: *Aerotow speed: *Winch launch max speed: *Terminal velocity: with full airbrakes".
- HKS-1 numberBuilt "2".
- HKS-1 primeUnits%3F_ "met".
- HKS-1 ref "Sailplanes 1945-1965".
- HKS-1 related HKS-3.
- HKS-1 similarAircraft "*Schempp-Hirth SHK * Standard Austria".
- HKS-1 sinkRateMs "0.61".
- HKS-1 sinkRateNote "at - 2-seat , at - solo".
- HKS-1 spanM "19".
- HKS-1 stallSpeedKmh "65".
- HKS-1 stallSpeedNote "-2".
- HKS-1 type "Two seat experimental sailplane".
- HKS-1 wingAreaSqm "17.79".
- HKS-1 m "29".
- HKS-1 wingLoadingNote "flown solo 35 kg/m²".
- HKS-1 subject Category:German_sailplanes_1950–1959.
- HKS-1 type Aircraft.
- HKS-1 type MeanOfTransportation.
- HKS-1 type Product.
- HKS-1 type DesignedArtifact.
- HKS-1 comment "The HKS-1 was a German 19 span high performance two seat sailplane, designed around 1950 to use recent advances in laminar flow airfoils. To avoid premature transition from laminar flow caused by surface interruptions, the HKS-1 dispensed with hinged ailerons, flaps and spoilers and replaced them with a flexible trailing edge. Two were built, setting several records.".
- HKS-1 label "HKS-1".
- HKS-1 sameAs m.0j46sb0.
- HKS-1 sameAs Q5629998.
- HKS-1 sameAs Q5629998.
- HKS-1 wasDerivedFrom HKS-1?oldid=592001873.
- HKS-1 isPrimaryTopicOf HKS-1.