Hanriot HD.1
| GENERAL DATA | |||
| Type |
Fighter
|
||
| Manufacturer(s) | Hanriot |
||
| Prototype first flight | 1916 |
Introduction | June 1916 |
| Production | about 1200 |
Crew | 1 |
| Variants | |||
| Hanriot HD-1 | 110hp Le Rhône 9J engine, 1 Vickers machine gun | ||
| Hanriot HD-1 | 170hp Le Rhône 9R engine, 2 Vickers machine guns | ||
| Hanriot HD-2 | Aircraft transformed into seaplane, larger tail and floats instead of the fixed gear | ||
| Hanriot HD-12 | Carrier-borne single-seat fighter proposed in the single-seat squadron program for September 1919. | ||
| DIMENSIONS | |||
| Length | 5.85 m |
Empty Weight | 407 kg |
| Wingspan | 8.7 m |
Loaded Weight | 605 kg |
| Height | 2.94 m |
Max takeoff weight | 652 kg |
| Wing area | 18 m² |
Wing loading | ? kg/m² |
| ARMAMENT | ||||
| Guns | 1-2 × 0.303 in (7.7 mm) Vickers
MG * |
Ammunition Carried |
? |
|
| Other Armament | 8 x Le Prieur rockets intended
for the destruction of Drachens |
|||
(*) forward of cockpit, synchronized / An 11 mm (0.433 in) Vickers gun on one or two Belgian machines.
| POWERPLANT | |||
| Engine | 1 ×
Le Rhône 9J then 9R |
Type & Displacement | Nine-cylinder air-cooled radial,
15 L |
| Horsepower | 109 hp then 170 hp |
Power/Weight Ratio | 180.165 hp then 280.99 hp/ ton * |
| Fuel Capacity | ? L
|
||
(*) with the loaded weight
| PERFORMANCES | |||
| Maximum Speed | 184 km/h |
Rate of Climb | 6.53 m/s |
| Range | 550 km |
Service Ceiling | 6400 m |
| Sources | |||
| Wikipédia (fr) | - | ||
Drawings |
