Sunward ST

{{Short description|Chinese ultralight trike}}

{{Use dmy dates|date=March 2018}}

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

{{Infobox aircraft begin

| name= ST

| image=

| caption=

}}{{Infobox aircraft type

| type=Ultralight trike

| national origin=China

| manufacturer=Sunward Tech

| designer=

| first flight=

| introduced=

| retired=

| status=In production (2018)

| primary user=

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| variants with their own articles=

}}

The Sunward ST is a Chinese ultralight trike designed and produced by Sunward Tech (Hunan Sunward Science & Technologies Company Limited) of Zhuzhou. The aircraft is supplied complete and ready-to-fly.Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 242. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

Design and development

The ST was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of {{convert|450|kg|lb|0|abbr=on}}. The aircraft has a maximum gross weight of {{convert|450|kg|lb|0|abbr=on}}.

The aircraft design features a strut-braced topless hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit with a cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.

The aircraft is made from bolted-together aluminum tubing and composites. It uses a double surface Grif Hazard wing, made by the Italian company Grif Italia. The {{convert|10.38|m|ft|1|abbr=on}} span wing is supported by struts and uses an "A" frame weight-shift control bar. The powerplant is an Austrian-made twin cylinder, liquid-cooled, two-stroke, dual-ignition {{convert|64|hp|kW|0|abbr=on}} Rotax 582 engine or four cylinder, air and liquid-cooled, four-stroke, dual-ignition {{convert|80|hp|kW|0|abbr=on}} Rotax 912UL engine.

The Rotax 582-equipped model has an empty weight of {{convert|198|kg|lb|0|abbr=on}} and a gross weight of {{convert|450|kg|lb|0|abbr=on}}, giving a useful load of {{convert|252|kg|lb|0|abbr=on}}. With full fuel of {{convert|60|L}} the payload is {{convert|209|kg|lb|0|abbr=on}}.

Variants

;ST582

:Model powered by a Rotax 582 two-stroke powerplant. Designed for flight training and aerial work, an agricultural aircraft version was introduced in 2012 with crop-spraying gear. This includes a {{convert|120|kg|lb|0|abbr=on}}-capacity tank that can cover {{convert|13.34|sqkm|sqmi|0|abbr=on}}.

;ST912

:Model powered by a Rotax 912UL four-stroke powerplant.

Specifications (ST582)

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|capacity=one passenger

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|empty weight kg=198

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|gross weight kg=450

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|fuel capacity={{convert|60|L}}

|more general=

|eng1 number=1

|eng1 name=Rotax 582

|eng1 type=two-cylinder, liquid-cooled, two stroke aircraft engine

|eng1 kw=48

|eng1 hp=

|prop blade number=3

|prop name=composite

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|max speed kmh=105

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|cruise speed kmh=80

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|stall speed kmh=40

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|wing loading kg/m2=27.8

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}}

See also

References

{{reflist}}