Heinkel He-112
| GENERAL DATA | |||
| Other Designation(s) | - |
||
| Type | Fighter |
Crew | 1 |
| Manufacturer(s) |
Heinkel |
||
| Production | 103 |
||
| First Flight | September 1935 |
Introduction | 1938 |
| Variants | |||
| He-112 V1 | Initial Prototype with. a Rolls-Royve Kestrel Mk.IIS of 695 hp. | ||
| He-112 V2 | Second prototype with a Junkers Jumo 210C of 640 hp and redesigned with thinner wings. | ||
| He-112 V3 | Third prototype with larger vertical stabilizer, radiator and spine. | ||
| He-112 V4 | Fourth prototype with Junkers Jumo 210Da of 690 hp and smaller vertical stabilizer. | ||
| He-112 V5 | Similar to V4 with 2 x 7.92 mm MG17 in fuselage. | ||
| He-112 V6 | Prototype with Junkers Jumo 210C and modified radiator. | ||
| He-112 V8 | Prototype with Daimler-Benz
DG600Aa of 910 ho. |
||
| He-112A-0 | Production Designation | ||
| He-112A-01 | Carrier borne version similar to V6 with Jumo 210C. | ||
| He-112A-02 | Similar to V6 with Jumo 210C. | ||
| He-112A-03 | Similar to V6 with Jumo 210C. Primarily an air-show aircraft. | ||
| He-112A-04 | Similar to V6 with Jumo 210C. Test Bed Model for Heinkel. | ||
| He-112A-05 | Similar to V6 with Jumo 210C, for Japan. | ||
| He-112A-06 | Similar to V6 with Jumo 210C, for Japan. | ||
| He-112B | Redesigned Prototype with 2 x 7.92 mm MH 17 in cowling sides and 2 x 20 mm MG FF guns in wings, redesigned enclosed bubble canopy, redisigned fuselage and rudder/Stabilizer. | ||
| He-112B V7 | With Daimler-Benz 600Aa engine. | ||
| He-112B V9 | With Junkers Jumo 210Ea engine of 680 hp and sublte aerodynamic changes. | ||
| He-112B V10 | With Daimler-Benz 601Aa engine of 1175 hp. | ||
| He-112B V11 | With Daimler-Benz 601Aa engine of 1175 hp. | ||
| He-112B V12 | Last prototype with fuel-injected 210Ga engine of 700 hp. | ||
| He-112B-0 | Production Model with 210C engines. | ||
| He-112B-1 | Production Model with 210Ea engines. | ||
| He-112B-2 | Production Model with 210Ga engines. | ||
| DIMENSIONS | |||
| Length | 9 m |
Empty Weight | 1680 kg |
| Wingspan | 11.5 m |
Loaded Weight | ? kg |
| Height | 3.7 m |
Max takeoff weight | 2230 kg |
| Wing area | 23.2 m² |
Wing loading | 102.5 kg/m² |
| ARMAMENT | ||||
| Main Gun | Wings | 2 × 20mm Oerlikon MG FF |
Ammunition Carried | 2 x 60 |
| Secondary Guns | Engine Cowling | 2 x 7.92 mm MG 17 |
Ammunition Carried | 2 x 500 |
| Others | 6 x 10 kg C-1 bomb |
|||
| POWERPLANT | |||
| Engine | 1 ×
Junkers Jumo 210Da/C |
Type & Displacement | liquid-cooled inverted V12, 19.7
L |
| Horsepower (maximum) | 689
hp / 700 hp (C) |
Power/Weight Ratio | 308.97 hp / ton * |
| Fuel Capacity | ?
L (internal)
|
||
(*) with maximum takeoff weight
| PERFORMANCES | |||
| Maximum Speed | 488-510
km/h at 3500 m |
Cruise Speed | 475 km/h |
| Stall Speed * | ? km/h |
Service Ceiling | 8000-9500 m |
| Rate of Climb | ? m/s |
Range | 1150 km |
(*) vitesse de décrochage
| Sources | |||
| Wikipédia | - | - |
|
Drawings |
