Häfeli DH-3

{{Infobox aircraft

|name = DH-3

|image = Der Doppeldecker wird in Position geschoben - CH-BAR - 3239658.tif

|caption =

|type = Reconnaissance biplane

|manufacturer = K+W

|designer = August Häfeli

|first_flight =

|introduction = 1917

|retired = 1939

|status =

|primary_user = Swiss Air Force

|more_users =

|produced =

|number_built = DH-3 24
DH-3a 83
DH-3b 3

|unit cost =

|developed_from = Hafeli DH-2

|variants =

}}

The Häfeli DH-3 was a 1910 Swiss two-seat reconnaissance aircraft, built by the aircraft department of the Federal Construction Works (Eidgenoessische Konstruktionswerkstaette, (K+W)) at Thun, Switzerland.

Development and design

Following the poor performance of the DH-2, August Häfeli designed an improved version the Häfeli DH-3. It was basically the same airframe as the DH-2, the upper wing had a cutout to give a greater field of fire for the pivoting machine gun.

It was a two-bay aircraft of wood and fabric construction, powered by a 120 hp (89 kW) Argus As II water-cooled inline engine. Initial problems with the landing gear and the engine cooling system led to modifications. Further developments were the re-engined and improved DH-3a, and the DH-3b used for engine trials. Following successful trials with an installation of the Handley Page slats all surviving DH-3as were modified in 1932.

Operational history

On 8 January 1919 a DH-3 inaugurated the first Swiss air mail service between Zurich and Berne. A DH-3 aircraft failed a structural test in 1923 which caused the DH-3 to be withdrawn from service. The DH-3a, following modification, remained in service until 1939.

Variants

;DH-3

:Initial production version with Argus As II engine, 24 built.

;DH-3a

:Improved version with Hispano-Suiza HS-41 8Aa engines, four aircraft ordered in 1919. A second order for 30 aircraft was placed in 1919 with license-built engines, a third order for 49 aircraft being placed in 1925. Survivors were modified at Thun in 1932 with Handley Page slats and changes to allow crew to wear parachutes.

;DH-3b

:Three aircraft powered by the indigenous 150 hp (112 kW) LFW 0 engine developed by the Swiss Locomotive and Machine Works were built in 1918.

Operators

Specifications (DH-3a)

{{Aircraft specs

|ref=The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985){{cite book |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985)|publisher= Orbis Publishing}}

|prime units?=met

|crew=2

|length m=7.95

|span m=12.5

|upper span m=

|mid span m=

|lower span m=

|width m=

|height m=3.1

|wing area sqm=38

|aspect ratio=

|airfoil=

|empty weight kg=1587

|gross weight kg=1110

|max takeoff weight kg=

|fuel capacity=

|more general=

|eng1 number=1

|eng1 name=Hispano-Suiza 8Aa (HS-41)

|eng1 type=V-8 water-cooled piston engine

|eng1 hp=150

|prop blade number=2

|prop name=fixed-pitch propeller

|prop dia m=

|prop dia ft=

|prop dia in=

|prop dia note=

|max speed kmh=145

|max speed mach=

|cruise speed kmh=

|stall speed kmh=

|never exceed speed kmh=

|minimum control speed kmh=

|range km=400

|combat range km=

|ferry range km=

|endurance=

|ceiling m=4500

|g limits=

|roll rate=

|climb rate ms=

|time to altitude=

|wing loading kg/m2=

|fuel consumption kg/km=

|power/mass=

|more performance=

|guns= 1x flexible machine gun in the rear cockpit

|bombs=

}}

References

{{reflist}}