Blackburn Firecrest

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title: "Blackburn Firecrest" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["cancelled-military-aircraft-projects-of-the-united-kingdom", "blackburn-aircraft", "1940s-british-fighter-aircraft", "carrier-based-aircraft", "inverted-gull-wing-aircraft", "single-engined-tractor-aircraft", "low-wing-aircraft", "aircraft-first-flown-in-1947", "aircraft-with-retractable-conventional-landing-gear", "single-engined-piston-aircraft"] description: "WWII British naval strike fighter" topic_path: "geography/united-kingdom" source: "https://en.wikipedia.org/wiki/Blackburn_Firecrest" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0

::summary WWII British naval strike fighter ::

::data[format=table title="Infobox aircraft"]

Field	Value
name	B-48 Firecrest
image	File:Blackburn YA1 1st.png
type	Strike fighter
manufacturer	Blackburn Aircraft
first_flight	1 April 1947
primary_user	Fleet Air Arm
produced	1947
number_built	2 (prototypes)
developed_from	Blackburn Firebrand
::

|name= B-48 Firecrest |image= File:Blackburn YA1 1st.png |caption= |type= Strike fighter |manufacturer= Blackburn Aircraft |designer= |first_flight= 1 April 1947 |introduction= |retired= |status= |primary_user=Fleet Air Arm |produced=1947 |number_built=2 (prototypes) |unit cost= |developed_from= Blackburn Firebrand |variants=

The Blackburn B.48 Firecrest, given the SBAC designation YA.1, was a single-engine naval strike fighter built by Blackburn Aircraft for service with the British Fleet Air Arm during the Second World War. It was a development of the troubled Firebrand, designed to Air Ministry Specification S.28/43, for an improved aircraft more suited to carrier operations. Three prototypes were ordered with the company designation of B-48 and the informal name of "Firecrest", but only two of them actually flew. The development of the aircraft was prolonged by significant design changes and slow deliveries of components, but the determination by the Ministry of Supply in 1946 that the airframe did not meet the requirements for a strike fighter doomed the aircraft. Construction of two of the prototypes was continued to gain flight-test data and the third was allocated to strength testing. The two flying aircraft were sold back to Blackburn in 1950 for disposal and the other aircraft survived until 1952.

Design

The Firebrand required significant effort by Blackburn to produce a useful aircraft and the first discussions on a redesign of the aircraft with a laminar-flow wing took place in September 1943. The new wing was estimated to reduce the weight of the wing by 700 lb and increase the aircraft speed by 13 mph. The extent of redesign increased and this led to a new fuselage and other improvements. In October 1943, Blackburn's design staff, led by G.E. Petty, started work on this development of the Firebrand which led to Specification S.28/43 being issued by the Air Ministry on 26 February 1944 covering the new aircraft. The specification was designed around a Bristol Centaurus 77 radial engine with contra-rotating propellers that allowed the size of the rudder to be reduced.

The new design, given the company designation B.48, was known unofficially by Blackburn as the "Firecrest" but was always known by S.28/43, the Air Ministry specification. It was a low-winged, single-seat, all-metal monoplane. Aft of the cockpit the fuselage was an oval-shaped stressed-skin semi-monocoque, but forward it had a circular-section, tubular-steel frame. The cockpit of the Firecrest was moved forward and raised the pilot's position so that he now looked over the wing leading edge, and down the nose. The canopy was adapted from the Hawker Tempest fighter. It could be hydraulically folded in two places to allow more compact storage in the hangar decks of aircraft carriers. Four Fowler flaps were fitted to give good low-speed handling for landing and the wing had retractable dive brakes on both surfaces. In the course of the redesign the structure was simplified which reduced weight by 1400 lb and even after the fuel capacity was increased by 70 impgal the gross weight was still 900 lb less than that of the Firebrand.

Work on two prototypes was authorised in November 1943, but proposals for alternative engines delayed progress. In 1945, it was decided that as well as adding another Centaurus-engined prototype, there should be three prototypes with the Napier E.122 (a development of the Sabre) as Specification S.10/45. The Ministry believed that this would enable Blackburn to develop their knowledge of aerodynamic and structural design and support the engine development at Napier. However, it was found that the S.10/45 aircraft could only be balanced if the E.122 powerplant was placed behind the pilot. The necessary redesign and 1000 lb weight increase, coupled with the limited funds available to the Royal Navy, meant that it could no longer be justified and the S.10/45 was cancelled on 8 October. While in final design, the Centaurus 77 engine with contra-rotating propellers was cancelled in January 1946 and a conventional 2825 hp Centaurus 57 was substituted. This engine was found to require flexible mounts and was modified into the Centaurus 59. The vertical stabiliser and rudder had to be enlarged from 33 sqft to 41 sqft to counteract the new engine's torque. In September 1946 a strength analysis conducted by the Ministry of Supply revealed that the aircraft would require strengthening to serve as a strike fighter and that a costly redesign would be required to bring it up to requirements, making it comparable in weight and performance to the Westland Wyvern which had already flown so no contract was placed for production aircraft.

Delayed by the late delivery of its propeller, the first prototype was rolled out at Brough in February 1947 and then taken by road to RAF Leconfield where it made its maiden flight on 1 April that year. All three prototypes were completed by the end of September 1947 and the third prototype had been modified to reduce the outer-wing dihedral to 3°. Both the second and third prototypes remained unflown when the Ministry of Supply ordered that flying be ceased and work on the aircraft be stopped. Later in the month, however, the third prototype was allocated to tests of powered aileron controls, as testing of the first prototype had shown that while adequate at cruise speed, the ailerons were heavy both at low and high speed. The second prototype was allocated to structural testing.

The third prototype made its maiden flight in early 1948, but the pace of the flight testing was leisurely with only 7 hours and 40 minutes completed by 30 November, over half of which were connected with air show performances. Testing concluded in March 1949 when the officer in charge concluded that there was no further purpose to the tests. While the Firecrest was faster than the Firebrand, and gave its pilot a much better view from the cockpit, it was otherwise disappointing, with test pilot and naval aviator Captain Eric Brown claiming that the Firecrest was even less manoeuvrable than the sluggish Firebrand, while the powered ailerons gave lumpy controls, leading to instability in turbulent air.

Operational history

::figure[src="https://upload.wikimedia.org/wikipedia/commons/0/0a/Blackburn_Firecrest.png" caption="Firecrest third prototype VF172"] ::

Operational experience had found Blackburn's Firecrest strike fighter to be far from suited to carrier operations. In particular, the pilot sat near the wing's trailing edge, looking over a very long and wide nose which gave a particularly poor view for landing. The Firecrest had also been rendered obsolete by the arrival of gas turbine engines, and while Blackburn did draw up proposals for turboprop-powered derivatives of the Firecrest (as the B-62 (Y.A.6) with the Armstrong Siddeley Python engine), these went unbuilt, with orders instead going to Westland for the Wyvern. The two flying prototypes remained in use until 1949, being sold back to Blackburn in 1950, and were later scrapped.

Aircraft

RT651 :One of two prototypes ordered on 1 January 1944 to Specification S.28/43. The airframe was sold by the Controller of Supplies (Air) to Blackburn on 17 April 1950.

RT656 :The second prototype ordered on 1 January 1944, it was used for structural testing before being disposed of in 1952.

VF172 :Third aircraft ordered on 18 April 1945 and it was used for research into power-boosted ailerons during February 1948. The airframe was sold to Blackburn on 17 October 1949.

Three further prototypes were ordered on 1 May 1945 against Specification S.10/45 and powered by Napier E.122 engine, but the order was cancelled and the aircraft were not built.

Specifications (Blackburn Firecrest)

|ref=The Incomplete Guide to Airfoil Usage; "Something Useful! Blackburn's 'Firecrest', Son of Firebrand"; Blackburn Aircraft Since 1909 |prime units?=imp General characteristics

|crew=1 |length ft=39 |length in=3.5 |span ft=44 |span in=11.5 |width ft=18 |width note=folded |height ft=14 |height in=6 |wing area sqft=361.5 |aspect ratio= |airfoil=root: NACA 43017 mod; tip of centre section NACA 66,2-(25)17; tip: NACA 64,2-(35)15 |empty weight lb=10513 |gross weight lb=15280 |max takeoff weight lb=16800 |fuel capacity=236 impgal internal fuel, with provision for 2× 45 impgal drop tanks under the wings and/or 1× 10 impgal drop tank on the centreline |more general= Powerplant

|eng1 number=1 |eng1 name=Bristol Centaurus 59 |eng1 type=18-cylinder air-cooled radial piston engine |eng1 hp=2825 |eng1 note=with Water/Methanol injection for take-off

|prop blade number=5 |prop name=Rotol constant-speed propeller |prop dia m=2.74 |prop dia ft=9 |prop dia note= Performance

|max speed mph=380 |max speed note=at 19000 ft |cruise speed mph=213 |cruise speed note=at 15000 ft |stall speed kmh= |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |range miles=900 |range note=at cruise |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance= |ceiling ft=30350 |ceiling note=service ceiling |g limits= |roll rate= |climb rate ftmin=2100 |climb rate note=initial r.o.c.

• Take-off run: 430 ft in 25 kn wind
• Landing run: 130 yd in 5 mph wind |time to altitude= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |fuel consumption kg/km= |fuel consumption lb/mi= |power/mass= |more performance= Armament -- |guns=Provision for 2 × 0.5 in M2 Browning machine guns under or in wing (not fitted to prototypes) |bombs=
  • 1 × 2097 lb torpedo, or
  • 2 × 250 lb bombs, one under each wing, in lieu of torpedo |rockets=8 × RP-3 rocket projectiles on underwing rails

|avionics=

Notes

References

Bibliography

• Brown, Eric. "The Firebrand...Blackburn's Baby 'Battleship'". Air International, July 1978, Vol. 15:1. pp. 25–31, 46–47. .
• Buttler, Tony. British Secret Projects: Fighters & Bombers 1935–1950. Hinckley, UK: Midland Publishing, 2004. .
• Buttler, Tony. "Something Useful! Blackburn's 'Firecrest', Son of Firebrand". Air Enthusiast. No. 82, July/August 1999. pp. 55–59. .
• Jackson, A. J. Blackburn Aircraft Since 1909. London: Putnam, 1968. .
• Mason, Francis K. The British Fighter Since 1912. Annapolis, Maryland: Naval Institute Press, 1992. .
• Sturtivant, Ray. Fleet Air Arm Fixed-Wing Aircraft Since 1946. Tonbridge, Kent, UK: Air-Britain, 2004. .

References

1. "Blackburn B-48 Firecrest Blackburn B-48 Firecrest".
2. Buttler 2004, pp. 181–182.
3. Jackson 1968, p. 452.
4. Mason 1992, pp. 330–331.
5. Buttler 1999, p. 55
6. In the rear fuselage was a single {{cvt. 52. impgal. USgal l fuel tank with two {{cvt. 92. impgal. USgal l fuel tanks in the centre wing section. The aircraft had a redesigned, thinner, inverted [[gull wing]] of laminar flow [[aerofoil section]]. The wing consisted of a two-[[spar (aviation). spar]] centre section with just over 6.5° of [[Dihedral (aeronautics)
7. Buttler 2004, p. 181.
8. Buttler 1999, pp. 56–58.
9. Buttler 1999, pp. 57–58.
10. Buttler 1999, pp. 58–59.
11. Brown 1978, p. 47.
12. Brown 1978, p. 46.
13. Buttler 1999, p. 59.
14. Sturtivant 2004, pp. 41-43.
15. Selig

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