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  • Text by Greg Goebal Thanks
    There were a number of proposals for Mosquito derivatives. In November 1941, DH proposed the "DH.99", later redesignated the "DH.101", fast heavy bomber to the Air Ministry. The DH.101 was apparently something like a scaled-up Mosquito that was to be powered by twin Napier Sabre 24-cylinder inline engines, used on the Hawker Typhoon, driving contrarotating propellers. It was informally referred to as the "Sabre Mosquito".

    The DH.101 was to carry a 7,260 kilogram (16,000 pound) bomb load to Berlin at a top speed of 692 KPH (430 MPH). However, the Sabre development program was troubled and DH was told they would have to make do with the Griffon, Rolls-Royce's next-generation successor to the Merlin. That configuration did not have clear advantages over the existing Mosquito and so the idea was dropped in April 1942. The Air Ministry then tossed around the notion of an improved "DH.102 Mosquito II" with two-stage Merlins, but de Havilland couldn't come up with a design concept that was particularly exciting, and that line of investigation was dropped in turn at the end of 1942.

    However, during 1942, DH had begun a private investigation of a single-seat fighter based on the Mosquito. The "DH.103 Hornet", as it would be known, was intended for the Pacific theater, where the great ocean spaces demanded long range, meaning a big fighter with a large fuel capacity. Air Ministry interest seemed muted and the DH.103 was shelved for a time, but excitement over the concept picked up in the spring of 1943, leading to an order for two prototypes in June 1943 under Specification "12/43".
    Below first prototype
    915
    Below 2nd prototype


    The first prototype performed its initial flight on 28 July 1944, with Geoffrey de Havilland JR at the controls. The prototype was in the air only 13 months after the beginning of the detailed design effort. The first flight was troublesome -- the undercarriage didn't want to retract and the aircraft suffered from serious tail buffeting -- but the problems were worked out. Performance exceeded predictions, with a top speed of 780 KPH (485 MPH) and a blazing climb rate of 1,370 meters (4,500 feet) per minute. A production order followed.

    As it emerged, the Hornet had an unmistakeable resemblance to the Mosquito, but was smaller and "sportier". The fuselage was built of wood in much the same way as the Mosquito, but the two-spar, one-piece, laminar-flow wing was of mixed construction, with a wood and metal internal structure, an undersurface of reinforced Alcad, and a birch-ply upper skin. The Hornet was the first aircraft to feature "wood bonded to metal" construction, using a new "Redux" adhesive.

    The Hornet was powered by twin Rolls-Royce Merlins, which unlike the Merlins fitted to the Mosquito were "handed", with a "Merlin 130" on one side and a "Merlin 131" on the other, both rated at 1,515 kW (2,030 HP) and fitted with Hydromatic four-blade variable-pitch propellers. The engine radiators were fitted in the leading edge of the wings inboard of the engines. Like the Mosquito, the Hornet had tailwheel landing gear, with the main gear retracting back into the engine nacelles and a semi-retractable tailwheel.
    Merlin
    The fighter was armed with four 20 millimeter Hispano cannon, fitted under the nose. The pilot sat under a backwards-sliding bubble-type canopy. The second prototype and production aircraft were fitted for underwing stores, including two 909 liter (200 Imperial gallon / 240 US gallon) drop tanks; or two 450 kilogram (1,000 pound) bombs; or eight RPs; or two 225 kilogram (500 pound) bombs and four RPs. Since the production aircraft were fitted with operational kit, they were heavier and so slower than the prototypes, but not by much, with a top speed of 760 KPH (472 MPH).

    Production of the fighter began at de Havilland's Hatfield plant in late 1944, with the first "Hornet F.1" machines delivered to RAF Boscombe Down for pre-service evaluation on 28 February 1945. A total of 60 production F.1s was built. Early production machines demonstrated some longitudinal instability, leading to the fit of a forward tailfin fillet that was retrofitted to initial production. The dorsal fillet was retained in all other Hornet variants.

    First production machine was PX210 which flew on 1 March 1945 and the Mark 1 served only in the UK, lacking the range of later variants.


    Service Fighter 19, 41, 64, 65 Training 1335 CU; 226 OCU; CFS; ECFS Communications FCCS; 12 GCF; 1 OFU; Horsham St Faith SF Other CFE (AFDS); CGS; PRDU; RAE; TRE


    PX217
    PX217
    PX225
    An unarmed photo-reconnaissance variant, the "Hornet PR.2", was considered, with three prototypes converted from F.1s and five evaluation aircraft built before a production order for 55 machines was canceled.
    F Mark 3 The main fighter variant was provided with increased internal tankage (from 360 to 540 gals) plus a further 400 gals in underwing tanks. To improve lateral stability a dorsal fillet was introduced and provision was made for two 1,000lb bombs or eight 60lb RPs under the wings. It entered service with 19 Sqn in March 1948 and when replaced by jet types in the UK this variant, together with the FR4, served in Malaya and Hong Kong.
    Service Fighter 19, 33, 41, 45, 64, 65, 80 Training FETS; Hornet CU; RAFC Communications 1689 Flt; 12 GCF; 10 MU; 1 OFU; Linton on Ouse SF Other CFE



    Mk III PX362


    PX367
    1950s
    FR Mark 4 The Mark 4 was the last of the Hornets and it was used exclusively in the Far East. It was basically an F Mk 3 equipped for photo-reconnaissance with an F.52 camera displacing 21 gals of fuel. Some were built on the production line while others were F Mk 3 conversions.

    DE HAVILLAND HORNET F.3:
    _____________________ _________________ _______________________

    spec metric english
    _____________________ _________________ _______________________

    wingspan 13.72 meters 45 feet
    wing area 33.54 sq_meters 361 sq_feet
    length 11.18 meters 36 feet 8 inches
    height 4.32 meters 14 feet 2 inches

    empty weight 5,842 kilograms 12,880 pounds
    loaded weight 9,480 kilograms 20,900 pounds

    max speed at altitude 760 KPH 470 MPH / 410 KT
    service ceiling 10,670 meters 35,000 feet
    range with drop tanks 5,635 kilometers 3,500 MI / 3,045 NMI
    _____________________ _________________ _______________________
    Most of the Mark 3s served in Malaya from 1950 to 1955 to deal with the Communist insurgency there. Their long endurance gave them substantial loiter time over target areas, and they were extremely accurate in cannon, bomb, and rocket strikes. They were phased out with regrets in 1955 due to spares shortages. The Hornet was the last RAF piston-powered fighter to see operational service.

    Even before the flight of the first Hornet prototype, de Havilland had been considering a carrier-based version for the FAA. In late 1944, under specification "N5/44", three early-production Hornet F.1s were modified to naval standards, with Heston Aircraft performing the design work.

    PX212

    The first Sea Hornet prototype flew on 19 April 1945. This machine had high-drag flaps, yoke-style arresting gear, tail-down catapult hookups, stronger landing gear, plus a navalized radio and other kit. The second prototype was similar, while the third prototype added wings that folded hydraulically upward outboard of the engine intakes.

    The third prototype began carrier trials on the HMS OCEAN on 10 August 1945.
    1

    A production order for the "Sea Hornet F.20" followed. It was the Fleet Air Arm's first twin-engine, carrier-based fighter. It retained the four 20 millimeter Hispano cannon and underwing stores of its land-based cousin, though the FAA used half-size drop tanks, with a capacity of 455 liters (100 Imperial gallons / 120 US gallons). Dimensions were the same as for the Hornet, though the empty weight increased by about 250 kilograms (550 pounds). The only major difference in appearance from the Hornet was that the Sea Hornet had a camera port on each side of the rear fuselage for an optional oblique reconnaissance camera.

    The Sea Hornet F.20 reached formal Royal Navy service in June 1947 with Number 801 Squadron, and a total of 79 was built. The type performed its first carrier cruise in 1949, on the HMS IMPLACABLE, and served in operational roles until 1951, when it was replaced by the Hawker Sea Fury. Some F.20s lingered in second-line roles until 1955.
    1
    103 Hornet Sn VR851

    1947
    Approach
    1

    Malta
    Landing
    Banking
    20
    VR857

    The last Sea Hornet variant was the "PR.22" photo-reconnaissance machine, which was similar to the F.20 but featured either two F.52 cameras or a single Fairchild K.19B night-photography camera in the rear fuselage. The cannon were deleted, with the gun ports faired over. It could still carry underwing stores. Only 23 were built.
    Ports
    1
    TT202
    * In late 1945, the Royal Navy came up with an urgent requirement for a carrier-based, two-seat night fighter, under specification "N.21/45". Heston Aircraft modified two Hornet F.3s to meet the specification, adding an ASH radar thimble in the nose, flame dampers on the exhausts, a small bubble-type canopy on the rear fuselage for a navigator / radar operator, and a larger tailplane assembly to compensate for the second canopy.

    The result was the "Sea Hornet NF.21". It was slightly longer than the F.3 due to the thimble radome, and its empty weight was about a tonne more. Despite its role as a night fighter, it apparently could carry the same underwing offensive stores as other Hornets and Sea Hornets.

    A total of 80 NF.21s was built. The NF.21 served as the standard FAA night fighter, operating off the carriers HMS VENGEANCE, INDOMITABLE, and EAGLE. It was also used to fly as a "formation leader" for groups of strike fighters. The NF.21 was replaced in operational service by the Sea Venom in 1954, lingering for another year in the radar training role.


    1948

    1955
    481
    Below taken post war, Hornet and Lightning aircraft of Spartan Air Services Ltd. Ottawa.

    A total of 150 Sea Hornets was built to final end of production in 1951, for a grand total of 350 Hornets and Sea Hornets. Pilots found the type a joy to fly, like a "Grand Prix racer" as one pilot put it, but its wooden construction apparently didn't fare well under tropical conditions. Apparently no Hornet or Sea Hornet survives today, even as a static display. sad








     
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  • Cool thread, thanks Duggy! I know I've said this many times before but to me the Hornet is arguably the best looking piston engined military aircraft built, although the night fighter does look a little awkward.
     

  • As Eric "Winkle" Brown states:

    "My favourite piston engine (aircraft) is the de Havilland Hornet. For the simple reason it was over-powered. This is an unusual feature in an aircraft, you could do anything on one engine, almost, that you could do on two. It was a 'hot rod Mosquito' really, I always described it as like flying a Ferrari in the sky."

    And if Eric states that, then it must be true.
    smile

     

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