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Shenyang HU-2 Petrel

The Shenyang HU-2 Petrel is a Chinese self-launching motor-glider built by the Shenyang Sailplane Factory at Shenyang.[1]

HU-2 Petrel
Role Motor-glider
National origin China
Manufacturer Shenyang Sailplane Factory

Design

The Petrel is a two or three-seat self-launching motor-glider made from wood and fabric that looks like a conventional high-wing monoplane.[1] It is powered by a front-mounted 80 hp (60 kW) Limbach L 2000 E01 piston engine.[1]

Specifications

Data from Brassey's World Aircraft & Systems Directory 1996[1]

General characteristics

  • Crew: 2 or 3
  • Length: 7.02 m (23 ft 0 in)
  • Wingspan: 14.92 m (43 ft 11 in)
  • Wing area: 19.63 m2 (211.3 sq ft)
  • Aspect ratio: 11.34
  • Empty weight: 485 kg (1,069 lb)
  • Gross weight: 750 kg (1,653 lb)
  • Powerplant: 1 × Limbach L 2000 E01 piston engine , 60 kW (80 hp)

Performance

  • Maximum speed: 135 km/h (84 mph, 73 kn)
  • Stall speed: 60 km/h (37 mph, 32 kn)

References

Notes

  1. ^ a b c d Taylor 1996, p. 511

Bibliography

  • Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory. London, England: Brassey's. ISBN 1-85753-198-1.

shenyang, petrel, chinese, self, launching, motor, glider, built, shenyang, sailplane, factory, shenyang, petrelrole, motor, glidernational, origin, chinamanufacturer, shenyang, sailplane, factory, contents, design, specifications, references, notes, bibliogra. The Shenyang HU 2 Petrel is a Chinese self launching motor glider built by the Shenyang Sailplane Factory at Shenyang 1 HU 2 PetrelRole Motor gliderNational origin ChinaManufacturer Shenyang Sailplane Factory Contents 1 Design 2 Specifications 3 References 3 1 Notes 3 2 BibliographyDesign EditThe Petrel is a two or three seat self launching motor glider made from wood and fabric that looks like a conventional high wing monoplane 1 It is powered by a front mounted 80 hp 60 kW Limbach L 2000 E01 piston engine 1 Specifications EditData from Brassey s World Aircraft amp Systems Directory 1996 1 General characteristicsCrew 2 or 3 Length 7 02 m 23 ft 0 in Wingspan 14 92 m 43 ft 11 in Wing area 19 63 m2 211 3 sq ft Aspect ratio 11 34 Empty weight 485 kg 1 069 lb Gross weight 750 kg 1 653 lb Powerplant 1 Limbach L 2000 E01 piston engine 60 kW 80 hp Performance Maximum speed 135 km h 84 mph 73 kn Stall speed 60 km h 37 mph 32 kn References EditNotes Edit a b c d Taylor 1996 p 511 Bibliography Edit Taylor Michael J H 1996 Brassey s World Aircraft amp Systems Directory London England Brassey s ISBN 1 85753 198 1 Retrieved from https en wikipedia org w index php title Shenyang HU 2 Petrel amp oldid 1137276893, wikipedia, wiki, book, books, library,

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