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Aero-Kros MP-02 Czajka

November 01, 2023

The Aero-Kros MP-02 Czajka (English: Lapwing) is a Polish ultralight aircraft designed and developed by Aero-Kros of Krosno, introduced at the Aero show held in Friedrichshafen in 2009. The aircraft is supplied ready-to-fly.[1][2]

MP-02 Czajka
Role Ultralight aircraft
National origin Poland
Manufacturer Aero-Kros
HMS Aviation
First flight 2009
Introduction 2009
Status In production

Since March 2017 the design has been built by HMS Aviation, which is also located in Krosno, Poland.[3]

Design and development edit

The Czajka was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a cantilever high-wing, a two seats in side-by-side configuration enclosed cockpit, tricycle landing gear and a single engine in tractor configuration.[1][2]

The aircraft is made from carbon-fiber-reinforced polymer. Its 9.72 m (31.9 ft) span wing employs Fowler flaps to keep the stall speed low enough for the FAI microlight category. The standard engine provided is the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant which gives a cruise speed of 230 km/h (143 mph). The cockpit is 1.215 m (48 in) wide.[1][2]

Specifications (MP-02) edit

 
Aero-Kros MP-02 Czajka

Data from Bayerl and Tacke[1][2]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Wingspan: 9.72 m (31 ft 11 in)
  • Wing area: 10.2 m2 (110 sq ft)
  • Empty weight: 268 kg (591 lb)
  • Gross weight: 472.5 kg (1,042 lb)
  • Fuel capacity: 112 litres (25 imp gal; 30 US gal)
  • Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke, 75 kW (101 hp)

Performance

  • Maximum speed: 230 km/h (140 mph, 120 kn)
  • Cruise speed: 170 km/h (110 mph, 92 kn)
  • Stall speed: 65 km/h (40 mph, 35 kn)
  • Rate of climb: 6.5 m/s (1,280 ft/min)
  • Wing loading: 46.3 kg/m2 (9.5 lb/sq ft)

References edit

  1. ^ a b c d Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 16. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. ^ a b c d Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 14. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  3. ^ "kontakt – HMS Aviation". hmsaviation.pl. Retrieved 10 May 2017.[permanent dead link]

External links edit

 
Wikimedia Commons has media related to MP-02 Czajka.
  • Official website

November 01, 2023
aero, kros, czajka, english, lapwing, polish, ultralight, aircraft, designed, developed, aero, kros, krosno, introduced, aero, show, held, friedrichshafen, 2009, aircraft, supplied, ready, czajkarole, ultralight, aircraftnational, origin, polandmanufacturer, a. The Aero Kros MP 02 Czajka English Lapwing is a Polish ultralight aircraft designed and developed by Aero Kros of Krosno introduced at the Aero show held in Friedrichshafen in 2009 The aircraft is supplied ready to fly 1 2 MP 02 CzajkaRole Ultralight aircraftNational origin PolandManufacturer Aero KrosHMS AviationFirst flight 2009Introduction 2009Status In productionSince March 2017 the design has been built by HMS Aviation which is also located in Krosno Poland 3 Contents 1 Design and development 2 Specifications MP 02 3 References 4 External linksDesign and development editThe Czajka was designed to comply with the Federation Aeronautique Internationale microlight rules and US light sport aircraft rules It features a cantilever high wing a two seats in side by side configuration enclosed cockpit tricycle landing gear and a single engine in tractor configuration 1 2 The aircraft is made from carbon fiber reinforced polymer Its 9 72 m 31 9 ft span wing employs Fowler flaps to keep the stall speed low enough for the FAI microlight category The standard engine provided is the 100 hp 75 kW Rotax 912ULS four stroke powerplant which gives a cruise speed of 230 km h 143 mph The cockpit is 1 215 m 48 in wide 1 2 Specifications MP 02 edit nbsp Aero Kros MP 02 CzajkaData from Bayerl and Tacke 1 2 General characteristicsCrew one Capacity one passenger Wingspan 9 72 m 31 ft 11 in Wing area 10 2 m2 110 sq ft Empty weight 268 kg 591 lb Gross weight 472 5 kg 1 042 lb Fuel capacity 112 litres 25 imp gal 30 US gal Powerplant 1 Rotax 912ULS four cylinder liquid and air cooled four stroke 75 kW 101 hp Performance Maximum speed 230 km h 140 mph 120 kn Cruise speed 170 km h 110 mph 92 kn Stall speed 65 km h 40 mph 35 kn Rate of climb 6 5 m s 1 280 ft min Wing loading 46 3 kg m2 9 5 lb sq ft References edit a b c d Bayerl Robby Martin Berkemeier et al World Directory of Leisure Aviation 2011 12 page 16 WDLA UK Lancaster UK 2011 ISSN 1368 485X a b c d Tacke Willi Marino Boric et al World Directory of Light Aviation 2015 16 page 14 Flying Pages Europe SARL 2015 ISSN 1368 485X kontakt HMS Aviation hmsaviation pl Retrieved 10 May 2017 permanent dead link External links edit nbsp Wikimedia Commons has media related to MP 02 Czajka Official website Retrieved from https en wikipedia org w index php title Aero Kros MP 02 Czajka amp oldid 1113330032, wikipedia, wiki, book, books, library,

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