Hanriot HD.2
| GENERAL DATA | |||
| Type |
Float Fighter
|
||
| Manufacturer(s) | Hanriot |
||
| Prototype first flight | 1917 |
Introduction | 1917 |
| Production | 12 |
Crew | 1 |
| Variants | |||
| HD.2 | floatplane fighter with Clerget 9B engine | ||
| HD.2C | HD.2 with wheeled undercarriage (10 built for USN, plus 2 converted from HD.2 by French Navy) | ||
| HD.12 | fitted with wheeled landing gear, powered by a 170-hp Le Rhône 9R rotary piston engine. (1 built) | ||
| HD.27 | powered by a 180-hp Hispano-Suiza 8Ac engine. (1 built) | ||
| H.29 | powered by a Hispano-Suiza 8Ab engine and fitted for launch from a warship (2 built) | ||
| DIMENSIONS | |||
| Length | 7.00 m |
Empty Weight | 495 kg |
| Wingspan | 8.51 m |
Loaded Weight | ? kg |
| Height | 3.10 m |
Max takeoff weight | 723 kg |
| Wing area | 18.4 m² |
Wing loading | ? kg/m² |
| ARMAMENT | ||||
| Guns | 2 × 0.303 in (7.7 mm) Vickers
MG * |
Ammunition Carried |
2 x ? |
|
| Other Armament | - |
|||
(*) forward of cockpit, synchronized
| POWERPLANT | |||
| Engine | 1 ×
Clêrget 9B |
Type & Displacement | nine-cylinderair-cooled rotary,
16.29 L |
| Horsepower | 130 hp |
Power/Weight Ratio | 17.81 hp/ ton * |
| Fuel Capacity | ? L
|
||
(*) with the maximun takeoff weight
| PERFORMANCES | |||
| Maximum Speed | 182-200
km/h |
Rate of Climb | 6.53m/s |
| Range | 300 km |
Service Ceiling | 4800 m |
| Sources | |||
| Wikipédia (fr) | histoiredumonde.net | ||
Drawings |
