2016년 7월 31일 일요일

He 72 (plane)

He 72 (plane)

Heinkel He 72

Bkadet2.jpg

Heinkel He 72 カデット (Heinkel He 72 Kadett) is German single-engine wings of a biplane training plane of the 1930s.

Table of contents

Development

"カデット" was designed in 1933 to be equal to an official demand for the basic training plane. It was the biplane of the single figure prop スタッガード wing having all metal body of the opening-type cockpit, tail assembly with the prop, rigid undercarriage. The prototype was equipped with アルグス As 8B air-cooled engine of output 104kW (139 hp) [2].

The initial mass production batch of He 72A that was a first mass production type remained the As 8B engine, but the subsequent mass production type was equipped with アルグス As 8R of output 112kW (150 hp). As for He 72A, it was replaced He 72B which was a main mass production type equipped with an S ハルスケ Sh 14A star-shaped engine of output 120kW (160 bhp) [2].

He 72B was produced as land plane-shaped He 72B-1 and seaplane type He 72BW ゼーカデット (Seekadett) of the 双 float. The development type of private specifications became He 72B-3 エーデルカデット (Edelkadett) [2].

History of the use

"カデット" was placed on duty in the National Socialism aviation army corps before Luftwaffe was organized. This plane was used for an attack duty as basic training plane later in the independent Slovak air force in Luftwaffe [2].

Derivation type

  • He 72A カデット: An initial mass production type.
  • He 72B:
  • He 72B-1:
  • He 72B-3 Edelkadett: A civilian airplane type of He 72B-1. 30 production.
  • He 72BW ゼーカデット: The seaplane of the 双 float. Only as for the prototype.
  • He 72B which attached He 172 - NACA cowling. In 1934 only as for the trial manufacture.

Operational

Essential points (He 72B-1)

The source: "The Complete Encyclopedia of World Aircraft" [3]

Specifications

Performance

  • Excess prohibition speed: km/h (kt)
  • Maximum velocity: 185km/h (100 kn) 115mph
  • Cruising speed: 170km/h (92 kn) 106mph
  • Stalling speed: km/h (kt)
  • A ferry flight flying range: km (nautical mile)
  • A flying range: 475km (256 nmi) 295 mi
  • Service ceiling: 3,500m (11,485 ft)
  • The rate of climb: 3m/s (591 ft/min)
  • Take-off run distance: m (ft)
  • Landing run distance: m (ft)
  • Loading: kg/m2 (lb/ft2)
  • Power loading (propeller): kW/kg (hp/lb)


As for the commentary of the used unit, please see Wiki project aviation / physics unit.

Allied item

Source

  1. ^ Wood and Gunston 1977, p.179.
  2. ^ a b c d "The Complete Encyclopedia of World Aircraft" Editors: Paul Eden & Soph Moeng, (Amber Books Ltd. Bradley's Close, 74-77 White Lion Street, London, NI 9PF, 2002, ISBN 0-7607-3432-1), 1152 pp.
  3. ^ Editors: Paul Eden & Soph Moeng, 2002, ISBN 0-7607-3432-1, page 833
  • Wood, Tony and Bill Gunston. Hitler's Luftwaffe: A Pictorial History and Technical Encyclopedia of Hitler's Air Power in World War II. London:Salamander books,1977. ISBN 0-86101-005-1.

Outside link


This article is taken from the Japanese Wikipedia He 72 (plane)

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