Aircraft Manufacturing Company Ltd / Airco DH 2
A conventional two -bay biplane of pusher configuration, the fuselage was curved along the front and top surfaces with slab sides and a flat underside - and held the armament, pilot, controls, fuel and engine. The pilot sat in an open-air cockpit "tub". A single machine gun was fitted to the front of the fuselage. Fuel was held directly aft of the pilot in one tank, and ahead of the engine, the latter mounted to the extreme end of the fuselage rear with a two-blade wooden propeller. Wings were in a two-bay with parallel struts additionally held by cabling. Both upper and lower wings sported slight dihedral. The empennage tapered off to become a single vertical tail fin with a high-mounted horizontal plane affixed. The undercarriage was fixed in place and featured two large main landing gear wheels attached to the fuselage underside. The rear of the aircraft was supported by a simple tail skid.
Modifications were made to the nose of the nacelle; the ammunition was carried in drums on external racks on each side of the cockpit; and the revised fuel system comprised a gravity tank fitted either under or on top of the upper mainplane on the port side. Production models retained the Gnome engine, as comparative trials with a 110-hp Le Rhone 9J powerplant revealed that this gave an inferior performance.
Along the Western Front, the DH.2 had met her match by the new breed of German and Austro-Hungarian fighter by December 1916. On December 20th, 1916, five out of six DH.2s were lost in one aerial fight against just five Albatros D.III series fighters. Phasing out of the D.H.2 began in France in March 1917, though D.H.2s serving in Palestine with No 11 Squadron, and with No 47 Squadron and a joint RFC/RNAS squad-ron in Macedonia, had a slightly longer ser-vice life. Two were evaluated at Home Defence stations in Britain in 1917 but were unable to cope with the Zeppelin raiders.
![]() Replica:
Mason Airco DH 2
Airco DH.2
Engine: 1 x Gnome Monosoupape, 100hp
Wing span: 8.61 m / 28 ft 3 in
Length: 7.68m / 25 ft 2½ in
Height: 2.91 m / 9 ft 6½ in
Wing area: 23.13 sq.m / 249 sq.ft
Empty weight: 423 kg / 943 1b
Loaded weight: 654 kg / 1,441 lb
Fuel capacity: 26.3 gallon
Maximum level speed at sea level: 150 km/h / 93 mph / 81 kt
Maximum Range: 249 miles / 400km
Endurance: 2 hours 45 minutes
Rate-of-Climb: 545ft/min / 166m/min
Climb to 1830m /6,000ft: 11 minutes
Service Ceiling: 14,000 ft / 4270 m
Armament: 1 x 7.62mm forward-firing Lewis machine gun on flexible mount.
Crew: 1
Airco DH.2
Engine: 1 x Le Rhone 9J, 110 hp
Wing span: 8.61 m / 28 ft 3 in
Length: 7.68m / 25 ft 2½ in
Height: 2.91 m / 9 ft 6½ in
Wing area: 23.13 sq.m / 249 sq.ft
Empty weight: 455 kg / 1004 1b
Loaded weight: 702 kg / 1547 lb
Maximum level speed at sea level: 143 km/h / 92 mph
Maximum Range: 249 miles / 400km
Endurance: 2 hours 45 minutes
Rate-of-Climb: 545ft/min / 166m/min
Climb to 1830m /6,000ft: 11 minutes
Service Ceiling: 14,000 ft / 4270 m
Armament: 1 x 7.62mm forward-firing Lewis machine gun on flexible mount.
Crew: 1
Airco DH.2
Engine: 1 x Clerget 9Z, 110 hp
Wing span: 8.61 m / 28 ft 3 in
Length: 7.68m / 25 ft 2½ in
Height: 2.91 m / 9 ft 6½ in
Wing area: 23.13 sq.m / 249 sq.ft
Empty weight: 428 kg / 943 1b
Maximum take-off weight: 654 kg / 1,441lb
Maximum level speed at sea level: 150 km/h / 93 mph / 81 kt
Maximum Range: 249 miles / 400km
Endurance: 2 hours 45 minutes
Rate-of-Climb: 545ft/min / 166m/min
Climb to 1830m /6,000ft: 11 minutes
Service Ceiling: 14,000 ft / 4270 m
Armament: 1 x 7.62mm forward-firing Lewis machine gun on flexible mount.
Crew: 1
|