Congratulations, you've wasted your time describing wartime emergency projects, which have almost no relation to pre-war Fleet Air Arm plans, which if given an additional 5 years, would very likely have come into production. A Fleet Air Arm in this situation is likely to have fighters with Rolls-Royce Griffons in service, as can be seen in the various N.8/39, N.9/39 and NAD.925/39 proposals put forward before the war.
I'm sorry I don't have any more information about British naval fighter projects, I hope what I'm sending is useful.
You can find information about the Royal Navy specification N.9/39 here:
https://www.secretprojects.co.uk/threads/gloster-n9-39-single-seat-naval-fighter-project.18589/
and here:
https://www.google.com/search?q=Roy...guMbgHgAbCBwUyLTguMsgHNQ&sclient=gws-wiz-serp
I only have something about the Firefly, the extended specification (N.5/40) specifically the night fighter version:
In response to a Royal Navy requirement for a new night fighter successor to the Fairey
Fulmar, Fairey modified a
Firefly F. Mk I day fighter in February 1943 as prototype NF. Mk II (Z1831/G). The letter "G" indicated that the aircraft contained secret equipment that was to be protected by armed guards, but during the flight tests at Boscombe Down Test Centre the radar had not yet been installed, and it was necessary to replace it with ballast in the rear cockpit and dummy radar pods on the wings.
The prototype showed heavy longitudinal stability and, to compensate for the additional weight, the forward fuselage was lengthened by 15 inches, and the center of gravity was brought forward 1.7 inches.
In February 1944 some operational tests were conducted with the RN Squadrons Nos. 772 and 746 and night trials of the second prototype (Z1840) highlighted additional shortcomings: the wing pods turbulence generated at high speeds required the redesign of the tail surfaces and the ailerons to improve their handling characteristics. The long nose adversely affected the fighter deck landing, the landing light reflected from the propeller blinded the pilot during the approach and the pods drag slowed the airplane about 40 mph.
The FAA requirement included the use of radar with dual AI/ASV capability (Air Interception/Air-Surface Vessel) flying at low level over the sea and on a horizontal line scanning, with automatic target tracking.
To deliver on that requirement, the Telecommunications Research Establishment (TRE) developed the AIX radar operating on 3.2 cm wavelength (“X” means X-Band 3.75 to 2.4 cm wavelength).
The equipment was very heavy and required the use of an additional generator and two parabolic scanners, with 16 inches of diameter, packaged into pods on the leading edge of both wings.
It was expected that the AIX could operate indistinctly in AI mode (with 40 degrees beam width, -5 +5 degrees in elevation and 10 miles range) and in ASV mode (with -20 degrees in elevation and 40 miles range). But the double-scanning system was difficult to synchronize with the propeller speed because the pods had been mounted too close to the fuselage.
TRE had mistakenly calculated that this could happen with a short pulse length radar, but, in practice, the returning signals were partially blocked by the propeller arc.
The NF. Mk II had been initially envisaged as a relatively straight forward adaptation of the basic F. Mk I airframe, but the introduction of a number of changes prevented easy production on the assembly lines and only 37 airframes were built.
This type was never used operationally and was retrofitted as F. Mk. IA by FAA field maintenance units.
In the summer of 1944, the main concern of the Royal Navy was the low-level nightly attacks performed by German and Japanese torpedo-bombers equipped with ASV radars.
The availability of the American AN/APS-4 radar (ASH or AI Mk XV in British parlance) when the US Navy selected the AN/APS-6 for the Grumman F6F-5N, persuaded the Admiralty to order the modification of 236 F. Mk. I airframes into FR. Mk. I fighter- reconnaissance planes, with the APS-4 installed on the production lines, modified windscreen, IFF Mk. III and improved gyro gunsight.
The Sperry/Western Electric AN/APS-4 AI centimetric radar set with beacon function, weighed 180 lb., and could pick up fighters at 4.5 miles, bombers at 5 miles and battleships at 30 miles, operating in X-band at 3.2 cm wavelength.
It could be operated in three modes: manual (aimed by the pilot), search and intercept.
In search mode the scanner antenna executed a two-line scan and a four-line scan in interception mode.
The radar provided suitable indication for firing guns but was relatively fragile and aerobatics in dogfight were forbidden.
Though rather too complex for effective use in single-seat airplanes, operating with a dedicated navigator-radioman as a second crewman, it could be used in air-to-surface mode to spot surface and underwater vessels at sea, with a secondary air-to-air capability against torpedo-bombers flying at low level over the sea.
The compact unit and the 18-inch diameter parabolic scanner was carried in a pressurized fiberglass pod mounted below the engine cowling, with the readouts installed in the rear cockpit.
To enable the radar beam to clear the propeller arc, the pod was installed in a simple crutch pointing 5 degrees downwards.
Deliveries of the FR. Mk I dual fighters started late in 1944 and entered service on July 1, 1945, with the 816 Squadron RN on board HMS
Nairana, but the type never saw action during the Second World War.
The NF. Mk I night fighter variant was developed in parallel with the FR. Mk I. The only external differences between both types were the shrouded exhausts and the anti-dazzle shields mounted above the last three exhausts pipes.
In addition, one slave radar screen was installed in the front cockpit for the pilot. But the system was not very effective because, as expected, caused the deterioration of the pilot night vision when regularly looking onto the indicator tube.
Trials with the 746 Squadron RN were completed by August 1944.
During the weeks that followed the 'D-Day', the forces of the Allies neutralized in their advance numerous V-1 launch sites built by the Germans in northern France. When the units of the
Wehrmacht retreated eastward, the new frontiers of the Reich got progressively further away from London. The V-1s launched from central Netherlands, with its maximum range of only 240 km, could no longer reach the British capital.
The
Luftwaffe intended to continue its bombing offensive on July 9, 1944, launching the V-1 from the obsolete bombers Heinkel He 111 H-16 of the III./KG3. Taking off with great difficulty from the Dutch airfields of Gilze-Rijen and Venlo, the Heinkels ventured far into the North Sea to launch their missiles against English cities. These V-1s came from the east, thus taking by surprise the British defenders that expected them from the south. Until the end of the war in Europe the III./KG3 made just 300 launches, and it was a dangerous work as some V-1 exploded prematurely and crashed against the bombers after launching, because of turbulence.
From the strategic point of view, the low frequency of launches was useless and the Heinkels were easy prey for the all-weather interceptors that searched them over the sea, but some German bombers managed to escape the detection of the British
Chain Home early warning radars flying below six hundred feet and the AI radars of the
Mosquitoes and
Black Widows were not designed to detect aircraft flying so low over the sea.
In October 1944 several
Fireflies NF. Mk. I of the experimental Night Fighter Interception Unit undertook night patrols over the North Sea, alongside the
Mosquitoes NF. Mk. XVII of the No. 68 Squadron RAF.
In April 1945, the 1790 Squadron RN received 18 NF. Mk I night fighters on board the HMS
Vindex. The carrier sailed to Australia to take part in the
Operation Olympic, the invasion of Kyushu scheduled for November. But the war was ended sooner than expected and the fighter had no opportunity to fight against Japan.
The night fighter paint scheme of the 1790 Sqn. airplanes were overall Sky Grey (FS 34424) with disruptive pattern in Grey Green (FS 34096) applied over the upper surfaces and BPF ‘roundel & bar’ identification markings.
Fairey
Firefly Fr. Mk I - technical data
Wingspan: 44.5 ft. (13.56 m); length: 37.6 ft. (11.45 m); height: 13.6 ft. (4.15 m); wing area: 328 sq. ft. (30.47 sq. m); max weight: 14,488 lb. (6,563 kg); max speed: 304 mph (489 km/h); service ceiling: 28,000 ft. (8,536 m.); range (with two 90 Imp. gals drop tanks): 1,364 miles (2,195 km); power plant: one Rolls-Royce
Griffon II B twelve-cylinder Vee liquid-cooled engine rated at 1,730 hp.; armament: four wing mounted 20-mm Hispano cannons and eight 60 lb. RP-3 rockets.
