Lockheed Hudson
1938
Back to the Virtual Aircraft Museum
  NAVAL BOMBERVirtual Aircraft Museum / USA / Lockheed  

Lockheed Hudson

The Hudson was originally built to the order of the British government as a military conversion of the L.14 transport. The first Hudson flew on 10 December 1938. Production lasted from 1939 until June 1943, thousands being built and delivered to the British, Australian, New Zealand, Canadian, Netherlands, Chinese and US forces.

Six versions of the Hudson were delivered to the British government, the majority of which arrived by air across the Atlantic. The Hudson I was powered by two 745.2kW Wright GR-1820-G102A Cyclone engines driving Hamilton-Standard two-position propellers. It first entered service with Coastal Command, RAF in mid-1939. The Hudson II was similar to the Mk I but had Hamilton-Standard Hydromatic constant-speed propellers fitted.

The Hudson III represented the first major revision, having 894kW GR-1820-G205A Cyclone engines with Hydromatic propellers and a retractable rear-firing ventral gun position. Large numbers of the Hudson III were delivered to the RAF under Lease-Lend (resulting in the use of the USAAF designation A-29) with 894kW Wright R-1820-87 Cyclone engines. Like earlier Hudsons, the Mk III was basically a maritime-patrol bomber and reconnaissance aircraft, but A-29A were fitted with benches for troop carrying. A-29/29A were also used by the USAAF and by the US Navy (as PBO-1).

Powered by two Pratt & Whitney R-1830-SC3G Twin Wasp engines, the Hudson IV was produced for the RAAF, but a small batch was diverted to the RAF. These had the ventral gun removed but received a D/F loop aerial in a transparent blister. The Hudson V for the RAF had R-1830-S3G4G engines driving Hamilton-Standard two-position propellers and a retractable ventral gun (as fitted to the Mk III). The final version was the Hudson VI (designated A-28 by the USAAF) which was convertible to troop transport or cargo carrier with the turret removed.

After withdrawal from combatant service with the RAF, USAAF and US Navy, the Hudson continued to be used for miscellaneous duties, including transport, air/sea rescue, training, target-towing, etc. As a trainer for air gunners, the USAAF operated a special version with a Martin dorsal turret as the AT-18.

The Hudson III was the first aeroplane to be fitted to carry the British-developed Mk I airborne lifeboat. This lifeboat was first used operationally in May 1943 by an RAF air/sea-rescue squadron to rescue the crew of a downed bomber in the North Sea.

Lockheed Hudson


Specification 
 MODEL"Hudson" Mk.I
 ENGINE2 x Wright GR-1820-G-102A, 820kW
 WEIGHTS
    Take-off weight7938 kg17500 lb
    Empty weight5276 kg11632 lb
 DIMENSIONS
    Wingspan19.96 m65 ft 6 in
    Length13.51 m44 ft 4 in
    Height3.61 m11 ft 10 in
    Wing area51.19 m2551.00 sq ft
 PERFORMANCE
    Max. speed396 km/h246 mph
    Ceiling7620 m25000 ft
    Range3150 km1957 miles
 ARMAMENT4 x 7.7mm machine-guns, 635kg of bombs

3-View 
Lockheed HudsonA three-view drawing (756 x 936)

Comments 
Fred F Smeaton, fred.smeaton(@)nl.rogers.com, 22.07.2008

We have a Hudson ar the North Atlantic Museum in Gander, How meny more are their left in the world? Is there any parts available,such as insterment panel Bomb Bay doors

Do you have any comments about this aircraft ?

Name    E-mail


COMPANY
PROFILE



All the World's Rotorcraft


Virtual Aircraft Museum


All rhe World's Rotorcraft AVIATION TOP 100 - www.avitop.com Avitop.com