Trendak Tercel: Difference between revisions
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{{Short description|Polish autogyro}} |
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{{Use dmy dates|date=January 2022}} |
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{{Use American English|date=January 2022}} |
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{|{{Infobox |
{|{{Infobox aircraft begin |
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| name= Tercel |
| name= Tercel |
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| image=File:Trendak Tercel - Bdg Air Fair 13 5-2016.jpg |
| image=File:Trendak Tercel - Bdg Air Fair 13 5-2016.jpg |
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| caption= |
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}}{{Infobox |
}}{{Infobox aircraft type |
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| type=[[Autogyro]] |
| type=[[Autogyro]] |
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| national origin= |
| national origin=Poland |
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| manufacturer=[[Aviation Artur Trendak]] |
| manufacturer=[[Aviation Artur Trendak]] |
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| designer= |
| designer= |
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| primary user= |
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| more users= <!--Limited to three in total; separate using <br /> --> |
| more users= <!--Limited to three in total; separate using <br /> --> |
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| produced= |
| produced= 2014–present |
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| number built= |
| number built= |
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| program cost= <!--Total program cost--> |
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| unit cost=<!-- [[US$]] [[Euro|€]] [[Pound sterling|£]] (date) --> |
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| developed from= |
| developed from= |
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| variants with their own articles= |
| variants with their own articles= |
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The '''Trendak Tercel''' ({{ |
The '''Trendak Tercel''' ({{trans|a male [[falcon]]}}) is a Polish [[autogyro]] designed and produced by [[Aviation Artur Trendak]] of [[Jaktorów|Jaktorów-Kolonia]], Poland, introduced at the [[AERO Friedrichshafen]] show in 2014. The aircraft is supplied complete and ready-to-fly.<ref name="WDLA15">Tacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015-16'', page 190. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}</ref> |
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==Design and development== |
==Design and development== |
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The Tercel features a single main rotor, a two-seats-in [[side-by-side configuration]] in completely enclosed cockpit with a windshield, [[tricycle landing gear]] with [[wheel pants]] and a four cylinder, air-cooled, [[turbocharged]], [[intercooled]], twin [[carburetor]], [[four-stroke]], {{convert|122|hp|kW|0|abbr=on}} [[CA 912 ULT (RST)]] engine in [[pusher configuration]].<ref name="WDLA15"/> |
The Tercel features a single main rotor, a two-seats-in [[side-by-side configuration]] in completely enclosed cockpit with a windshield, [[tricycle landing gear]] with [[wheel pants]] and a four cylinder, air-cooled, [[turbocharged]], [[intercooled]], twin [[carburetor]], [[four-stroke]], {{convert|122|hp|kW|0|abbr=on}} [[CA 912 ULT (RST)]] engine in [[pusher configuration]].<ref name="WDLA15"/> |
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The aircraft [[fuselage]] is made from [[composite material]]. Its Trendak & Son aluminum, two-bladed rotor has a diameter of {{convert|8.4|m|ft|1|abbr=on}}. The aircraft has a typical empty weight of {{convert|285|kg|lb|0|abbr=on}} and a gross weight of {{convert|560|kg|lb|0|abbr=on}}, giving a useful load of {{convert|275|kg|lb|0|abbr=on}}. With full fuel of {{convert|120| |
The aircraft [[fuselage]] is made from [[composite material]]. Its Trendak & Son aluminum, two-bladed rotor has a diameter of {{convert|8.4|m|ft|1|abbr=on}}. The aircraft has a typical empty weight of {{convert|285|kg|lb|0|abbr=on}} and a gross weight of {{convert|560|kg|lb|0|abbr=on}}, giving a useful load of {{convert|275|kg|lb|0|abbr=on}}. With full fuel of {{convert|120|L}} in two tanks, the payload for the pilot, passenger and baggage is {{convert|189|kg|lb|0|abbr=on}}.<ref name="WDLA15"/> |
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==Specifications (Tercel) == |
==Specifications (Tercel) == |
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[[File:Trendak Tercel Pro at AERO Friedrichshafen 2018 (1X7A4523).jpg|thumb|Trendak Tercel Pro at AERO Friedrichshafen 2018]] |
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{{Aircraft specs |
{{Aircraft specs |
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|ref=Tacke<ref name="WDLA15"/><ref>{{cite web|url =http://www.trendak.eu/pl/modele/tercel/ |title = Tercel|accessdate = 7 October 2017|author=Aviation Artur Trendak |work = www.trendak.eu}}</ref> |
|ref=Tacke<ref name="WDLA15"/><ref>{{cite web|url =http://www.trendak.eu/pl/modele/tercel/ |title = Tercel|accessdate = 7 October 2017|author=Aviation Artur Trendak |work = www.trendak.eu}}</ref> |
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|gross weight lb= |
|gross weight lb= |
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|gross weight note= |
|gross weight note= |
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|fuel capacity={{convert|120| |
|fuel capacity={{convert|120|L}} in two {{convert|60|L}} tanks |
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|more general= |
|more general= |
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{{Commons category}} |
{{Commons category}} |
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*{{Official website|http://www.trendak.eu/pl/modele/tercel/}} |
*{{Official website|http://www.trendak.eu/pl/modele/tercel/}} |
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[[Category:Trendak aircraft|Tercel]] |
[[Category:Trendak aircraft|Tercel]] |
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[[Category:Polish sport aircraft |
[[Category:2010s Polish sport aircraft]] |
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[[Category:Single-engined pusher |
[[Category:Single-engined pusher autogyros]] |
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[[Category:Twin-boom aircraft]] |
Latest revision as of 10:31, 8 December 2024
Tercel | |
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Role | Autogyro |
National origin | Poland |
Manufacturer | Aviation Artur Trendak |
Introduction | 2014 |
Status | In production (2017) |
Produced | 2014–present |
The Trendak Tercel (transl. a male falcon) is a Polish autogyro designed and produced by Aviation Artur Trendak of Jaktorów-Kolonia, Poland, introduced at the AERO Friedrichshafen show in 2014. The aircraft is supplied complete and ready-to-fly.[1]
Design and development
[edit]The Tercel is one of three similar designs that were all unveiled at the same time and which share common components. The Twistair is a tandem development, while the Trooper is a military variant with sideways facing seats for troop transport.[1]
The Tercel features a single main rotor, a two-seats-in side-by-side configuration in completely enclosed cockpit with a windshield, tricycle landing gear with wheel pants and a four cylinder, air-cooled, turbocharged, intercooled, twin carburetor, four-stroke, 122 hp (91 kW) CA 912 ULT (RST) engine in pusher configuration.[1]
The aircraft fuselage is made from composite material. Its Trendak & Son aluminum, two-bladed rotor has a diameter of 8.4 m (27.6 ft). The aircraft has a typical empty weight of 285 kg (628 lb) and a gross weight of 560 kg (1,235 lb), giving a useful load of 275 kg (606 lb). With full fuel of 120 litres (26 imp gal; 32 US gal) in two tanks, the payload for the pilot, passenger and baggage is 189 kg (417 lb).[1]
Specifications (Tercel)
[edit]General characteristics
- Crew: one
- Capacity: one passenger
- Length: 4.9 m (16 ft 1 in)
- Width: 2.2 m (7 ft 3 in)
- Height: 2.8 m (9 ft 2 in)
- Empty weight: 285 kg (628 lb)
- Gross weight: 560 kg (1,235 lb)
- Fuel capacity: 120 litres (26 imp gal; 32 US gal) in two 60 litres (13 imp gal; 16 US gal) tanks
- Powerplant: 1 × CA 912 ULT (RST) four cylinder, air-cooled, turbocharged, intercooled, twin carburetor, four stroke aircraft engine, 91 kW (122 hp)
- Main rotor diameter: 8.4 m (27 ft 7 in)
- Main rotor area: 55.4 m2 (596 sq ft) Trendak & Son aluminum
- Propellers: 5-bladed Kaspar KA-2/3, 1.740 m (5 ft 9 in) diameter
Performance
- Maximum speed: 175 km/h (109 mph, 94 kn)
- Cruise speed: 140 km/h (87 mph, 76 kn) minimum speed 50 km/h
- Never exceed speed: 210 km/h (130 mph, 110 kn)
- Range: 800 km (500 mi, 430 nmi) no reserves
- Endurance: 6 hours
- Service ceiling: 4,500 m (14,800 ft)
- Maximum glide ratio: 3:1
- Rate of climb: 6.1 m/s (1,200 ft/min)
- Disk loading: 10.1 kg/m2 (2.1 lb/sq ft)