Weller ULI NG

{{Short description|German ultralight aircraft}}

{{Use dmy dates|date=January 2022}}

{{Use British English|date=January 2022}}

{{Infobox aircraft begin

| name=ULI NG

| image=File:D-MOHN - Weller ULI NG.jpg

| caption=

}}{{Infobox aircraft type

| type=Ultralight aircraft

| national origin=Germany

| manufacturer=Weller Flugzeugbau

| designer=

| first flight=

| introduced=2010

| retired=

| status=In production (2012)

| primary user=

| more users=

| produced=

| number built=

| developed from= Egon Scheibe Uli 1

| variants with their own articles=

}}

The Weller ULI NG (New Generation), sometimes called the Weller Uli NG, is a German ultralight aircraft, designed and produced by Weller Flugzeugbau of Bibersfeld. It was introduced at the Aero show held in Friedrichshafen in 2010. The aircraft is supplied as a complete ready-to-fly-aircraft.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 84. WDLA UK, Lancaster UK, 2011. {{ISSN|1368-485X}}Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 88. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

Design and development

The aircraft is derived from the Egon Scheibe Uli 1 and was re-designed to comply with the German {{convert|120|kg|lb|0|abbr=on}} class ultralight rules. It features a cable-braced high-wing, a single-seat open cockpit without a windshield, fixed conventional landing gear and a single engine in pusher configuration.{{cite web|url=http://www.weller-flugzeugbau.de/node/14/62 |title= Weller Uli NG |last=Weller Flugzeugbau |publisher=Weller-flugzeugbau.de |date= |accessdate=2012-09-13}}

The aircraft fuselage is made from welded steel tubing, the wing built from bolted-together aluminum tubing, with its flying surfaces covered in aircraft fabric. Its {{convert|9.68|m|ft|1|abbr=on}} span wing has an area of {{convert|12.78|m2|sqft|abbr=on}}, giving a very light wing loading of 17.0 kg/m2 (3.5 lb/sq ft). The standard engine available is the {{convert|30|hp|kW|0|abbr=on}} Briggs & Stratton industrial four-stroke powerplant with a V-belt reduction drive, powering a two bladed wooden propeller. The engine burns {{convert|5|L}} per hour at cruise. The aircraft's {{convert|18|L}} fuel tank is detachable for refueling and is filled with premium auto-fuel. The design incorporates a ballistic parachute whole-aircraft rescue system that includes an ignition cut-off upon firing.

Specifications (version)

{{Aircraft specs

|ref=Bayerl, Tacke and Weller

|prime units?=met

|genhide=

|crew=one

|capacity=

|length m=5.92

|length ft=

|length in=

|length note=

|span m=9.68

|span ft=

|span in=

|span note=

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=12.78

|wing area sqft=

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=119.5

|empty weight lb=

|empty weight note=

|gross weight kg=220

|gross weight lb=

|gross weight note=

|fuel capacity={{convert|18|L}} removable tank

|more general=

|eng1 number=1

|eng1 name=Briggs & Stratton

|eng1 type=two cylinder, air-cooled, four stroke aircraft engine, with a V-belt reduction drive

|eng1 kw=

|eng1 hp=30

|prop blade number=2

|prop name=wooden

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kmh=95

|max speed mph=

|max speed kts=

|max speed note=

|cruise speed kmh=80

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kmh=45

|stall speed mph=

|stall speed kts=

|stall speed note=

|never exceed speed kmh=

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

|range km=150

|range miles=

|range nmi=

|range note=

|endurance=2:30 plus reserve

|ceiling m=

|ceiling ft=

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=2

|climb rate ftmin=

|climb rate note=

|time to altitude=

|sink rate ms=

|sink rate ftmin=

|sink rate note=

|lift to drag=

|wing loading kg/m2=17.0

|wing loading lb/sqft=

|wing loading note=

|power/mass=

|thrust/weight=

|more performance=

|avionics=

}}

References

{{reflist}}