Heinkel He 72
|He 72 Kadett|
|Role||Military basic trainer|
|Status||out of service|
National Socialist Flyers Corps
Slovenské vzdušné zbrane
|Number built||Several thousand |
The Kadett was designed in 1933 to meet an official requirement for a basic trainer. It was a single-bay biplane of fabric-covered, metal construction with open cockpits, a staggered wing, a strut-braced tail unit, and fixed tailskid undercarriage. The prototype was powered by a 104 kW (139 hp) Argus As 8B air-cooled inline engine.
The first production model, the He 72A retained the As 8B engine in early batches, but later production aircraft had a 112 kW (150 hp) As 8R. The He 72A was superseded by the He 72B, which was the major production version. This was powered by a 120 kW (160 bhp) Siemens-Halske Sh 14A radial.
The Kadett entered service with National Socialist Flyers Corps before the formation of the Luftwaffe. Later, it became a standard basic trainer with the Luftwaffe. Slovak forces used it in the attack role.
- He 72A Kadett : Initial production version.
- He 72B :
- He 72B-1 :
- He 72B-3 Edelkadett : Civil adaptation of He 72B-1. 30 built.
- He 72BW Seekadett : Twin-float seaplane. Prototype only.
- He 172 - He 72B with NACA cowling. Prototype only in 1934.
- Czechoslovakian Air Force (Postwar)
- Imperial Japanese Navy - one aircraft
Specifications (He 72B-1)
Data from "The Complete Encyclopedia of World Aircraft" 
- Crew: Two
- Length: 7.50 m (24 ft 7¼ in)
- Wingspan: 9.00 m (29 ft 6¼ in)
- Height: 2.70 m (8 ft 10¼ in)
- Wing area: 20.70 m² (222.82 ft²)
- Empty weight: 540 kg (1,191 lb)
- Max. takeoff weight: 865 kg (1,907 lb)
- Powerplant: 1 × BMW-Bramo Siemens-Halske Sh 14A 7-cylinder radial engine, 119 kW (160 hp)
- Maximum speed: 185 km/h (100 kn, 115 mph)
- Cruise speed: 170 km/h (92 kn, 106 mph)
- Range: 475 km (256 nmi, 295 mi)
- Service ceiling: 3,500 m (11,485 ft)
- Rate of climb: 3 m/s (591 ft/min)
- Aircraft of comparable role, configuration and era
|Wikimedia Commons has media related to Heinkel He 72.|