Royal Aircraft Factory designations

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My Royal Aircraft Factory designation list likely duplicates what AM has already produced (alas, I can't open doc files). Anyway, an html version will be more searchable and, with luck, there will be some additions ...
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Royal Aircraft Factory Designations

The mandate of the Royal Aircraft Factory originally restricted its activities to the building (or rebuilding) of experimental designs. Initial RAF designations combined an airframe layout type with 'Experimental'.

The layout types were named after individual aircraft designers -- S.E. (Santos Experimental after Alberto Santos-Dumont) for canards, B.E. (Bleriot Experimental after Louis Blériot) for tractor propeller designs, and F.E. (Farman Experimental after Henri Farman) for pusher propeller types.

By 1913/1914 the layout type designations were abandoned in favour of role designators. The F.E. and S.E. designations were retained but with new meanings.

Role letter combinations were: A.E. (Armed Experimental), C.E. (Coastal Experimental), F.E. (Fighting Experimental), N.E. (Night-flying Experimental), R.E. (Reconnaissance Experimental, S.E. (Scout Experimental).

An exception was the in-production B.E. series (which remained Blériot Experimentals). An anomoly was the B.S. series which combining the Blériot name with the Scout role. A.T. (Air Target) fits the role letter series ... except that the name was a counter-espionage cover designation.

Harder to explain are the unbuilt T.E. series. The original T.E. (Tatin Experimental) was named after the tail pusher-prop configuration of Victor Tatin's 1911 Aero-Torpille design). But the later T.E.1 concept was an enlarger S.E.5a fighter. In the latter case, the T.E. may have stood for 'Tractor Experimental' -- an attempt at rationalizing the RAF designation system?

For sub-types, suffix letters were applied. Older sources tend to render these suffixes as lower-case letters, later sources as capitals. I have stuck to lower-case. Royal Aircraft Factory engines were given type numbers after R.A.F. Here I have written engine types as 'RAF' as a space saver.

NB: For airships and balloon designations, see: Kites, Birds & Stuff: The Aviation Archive of the Royal Aircraft Factory + Inflatables by P.D. Stemp.
 
Royal Aircraft Factory Designations - A.E. and A.T. Series

A.E. Series - Armed Experimental

A.E.1 - 1913 experimental armed pusher biplane, 1 x 100 hp Chenu 6-cyl. inline
-- aka F.E.3, wire-braced tailboom extended from the centre of propeller hub

A.E.2 - Armoured nacelle tractor biplane design, likely not completed

A.E.3 - 2-seat armoured 'contact patrol' fighter, aka Farnborough Ram
- A.E.1: April 1918, 1st A.E.3 prototype, 212 hp Sunbeam Arab V8
-- A.E.1 aka Ram I
- A.E.2: June 1918, second A.E.3 prototype, 230 hp Bentley BR.2
-- A.E.2 aka Ram II
- A.E.3: July 1918, third A.E.3 prototype, 212 hp Sunbeam Arab

A.T. Series - Aerial Target

A.T. series - Aerial Target (radio-controlled, pilotless airplane) *
- * NB: 'Aerial Target' was really more of a cover designation

A.T. - [1] 1916-17 shoulder-wing monoplane flying bomb/Zeppelin defence
- A.T.: [1] span 6.7m, 1 x 35hp [30hp?] ABC Gnat air-cooled HO 2-cyl
-- A8957 to A8962, first flight 06 July 1917 (first 3 A.T.s crashed)
- A.T.: [1] aka Ruston Proctor* Aerial Target, designed by H P Folland
-- * WWI aero-engine builder Ruston & Proctor also constructed B.E.2s

A.T. - [2] 1920-21 pilotless A.T. [1] development
- A.T.: [2] 45hp Armstrong Siddeley Ounce air-cooled HO 2-cyl

A.T. [??] - Manned conv. (B8962) by No 3 (Western) Aircraft Depot, Bristol
-- Manned conv. fitted with ailerons and wheels repl. skid undercarriage

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Royal Aircraft Factory Designations - B.E., B.S., and C.E. Series

B.E. Series - British Experimental, orig. Blériot Experimental
[Variously given as Biplane or Blériot Biplane Experimental]

B.E.1 --- 1911 experimental tractor biplane, 60 hp Wolseley V8, 1 built

B.E.2 --- 1912 2-seat reconnaissance biplane, follow-on from B.E.1 prototype
- B.E.2 : 1912 experimental biplane prototype, 60 hp Renault V8
- B.E.2a: 1912 series 2-seat reconnaissance biplane, ~100 built
- B.E.2b: 1912 recce biplane, later a/c with ailerons in place of wing-warping
- B.E.2c: 1914 recce biplane, new horiz. tail + staggered wings with ailerons
-- night-fighter B.E.2c flown as single-seater (aux. fuel tank in fwd cockpit)
- B.E.2d: dual-control trainer version of '2c, used operationally by Belgium
-- Hispano-powered Belgian B.E.2d flown from front cockpit with gunner behind
- B.E.2e: 'Quirk' recce aircraft, B.E.2c with new, single-bay wings
- B.E.2f: as per B.E.2c but fitted with '2e style single-bay wings
- B.E.2g: as per B.E.2d but fitted with '2e style single-bay wings

B.E.3 --- 1912 (03.05.1912) experimental tractor biplane, 1 x 50hp Gnome rotary
- B.E.3: Featured reverse staggered wings with fuselage attached to upper wing

B.E.4 --- 1912 experimental training biplane, sim. to B.E.3, x 3 (or poss. 4)

B.E.5 --- 1912 third B.E.1/2 prototype, 60 hp ENV 'F' (then Renault V8), x 1

B.E.6 --- 1912 fourth B.E.1/2 prototype, 60 hp ENV 'F' (then Renault V8)
-- Officially claimed to be a rebuild of crashed S.E.1 (hence ENV 'F' engine)

B.E.7 --- 1913 B.E.3/4 devel., shortened fuselage, 140hp twin-row Gnome, 1 built

B.E.8 --- 1913 rotary-engined B.E.3/4/7 follow-on with low-set fuselage
- B.E.8 : initial production model 2-seat recce biplane, 80 hp Gnome rotary
-- B.E.8 series production ordered from Vickers, COW, and BCAC (Bristol)
- B.E.8a: 1915 dev. with B.E.2c wings, Gnome or Clerget 7Z rotary engine

B.E.9 -- 1915 exper. 2-seat recce-fighter with gunner ahead of propeller
- B.E.9 : 1915 prototype (essentially a modifified B.E.2c), 90hp RAF 1a V8
- B.E.9a: [Project] High-powered version, 140hp RAF 4a engine, not built

B.E.10 -- [Project] May 1914 B.E.2c with steel-tube fuselage, shorter wings
- B.E.10: Order for 4 prototypes from BCAC (Bristol) cancelled, none built

B.E.11 -- [Project] 1915, none built (no details, poss. a B.E.2 derivative)

B.E.12 -- 1915, single-seat recce-fighter der. from B.E.2c
- B.E.12 : 1915-16 series, 140 hp RAF 4a V12, 250 built
- B.E.12a: 1916 development with single-bay B.E.2e-style wings, 150 ordered
- B.E.12b: 200hp Hispano-Suiza V8, return to 2-bay B.E.2c wings, 100 ordered
-- note: some of the 100 B.E.12b ordered completed as RAF 4a-engined B.E.12s

B.S. Series - Blériot Scout

B.S.1 - 1913 tractor biplane recce scout, 1 x 100 hp Gnome 14 rotary

B.S.2 - Oct 1913 rebuilt B.S.1 prototype, 1 x 80 hp Gnome 7 rotary
- B.S.2: Enlarged vers. of B.S.1, may have had steel-tube fuselage

B.S.2 - [2] [Project] Original designation on R.E.1 design sketches*
-- * It is unclear whether 'both' B.S.2 types are one and the same

C.E. Series - Coastal Experimental

C.E.1 - 1918 2-seat coastal patrol flying boat, pusher engine, 2 built
- C.E.1 N.97: 1st prototype, late 1917, flown 17 Jan 1918, 1 x 230 hp RAF 3a V12
- C.E.1 N.98: 2nd prototype, 1918, 1 x 260 hp Sunbeam Maori V12 (14.7 Litres)

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Royal Aircraft Factory Designations - F.E. and H.R.E. Series

F.E. Series - Farman Experimental (later changed to Fighter Experimental)

F.E.1 - 1910 experimental biplane, 'Boxkite'-style open canard, 1 built
-- Design by de Havilland, 1 x pusher 45 hp Iris 4-cyl (also by de Havilland)

F.E.2 - 1911 experimental biplane, pusher engine, conv. tailplane, 1 built
-- claimed to be F.E.1 rebuild, 1 x 50 hp Gnome (repl. by 70 hp Renault)

F.E.2 - duplicate designation for 1914 two-seat pusher biplane series
- F.E.2 : officially 1911 F.E.2 rebuild, actually completely new design
- F.E.2a: 1915 'machine gun carrier', 120 hp Beardmore 6 cyl., 12 built
-- 1st prod. a/c fitted with 100 hp Green E.6, re-engined with Beardmore
- F.E.2b: 1915 recce-fighter, 120 hp then 160 hp Beardmore, 1211 built
- F.E.2c: 1916 exper. night fighter/bomber F.E.2b, pilot position fwd.
-- NB: F.E.2c desig. re-used for 1918 F.E.2b night bomber conversions
- F.E.2d: F.E.2b powered by 1 x 250 hp R-R Eagle V12, 386 built
- F.E.2e: experimental variant with alternative engine [type?]
- F.E.2f: experimental variant with alternative engine [type?]
- F.E.2g: experimental variant with alternative engine [type?]
-- Alt. engines included 284 hp R-R Eagle III and 200 hp RAF 3A
- F.E.2h: experimental variant with 230 hp BHP (Siddeley) Puma
-- NB: 100 F.E.2h (F9296-F9395) ordered from Garrett, cancelled
- VIM (Vickers Instructional Machines) 35 F.E.2 trainers for China, 1919

F.E.3 - 1913 experimental armed pusher biplane, 1 x 100 hp Chenu 6-cyl. inline
-- aka A.E.1, wire-braced tailboom extended from the centre of propeller hub

F.E.4 - 1916 3-seat twin-pusher ground attack biplane (COW 1 1/2-pdr), 2 built
- F.E.4 N.7993: 1st prototype, March 1916, 2 x 150 hp RAF 5a V12s
- F.E.4 N.7994: 2nd prototype, July 1916, 2 x 250 hp Rolls-Royce Eagle V12s
-- variants with 200 hp RAF 3a, 150 hp RAF.4a, 170 hp RAF 4b not pursued

F.E.5 - [Project] 1916/17 twin-fuselage heavy bomber combining F.E.4 fuselages
-- 1 x RAF 4A in the nose of each fuselage, RAF 5 pusher in centre lower wing

F.E.6 - 1914 2-seat pusher fighter, enl. F.E.3 with COW gun, 120 hp Austro-Daimler
-- 1 prototype, abandoned after tests, tail boom through the airscrew shaft

F.E.7 - [Project] 2-seat devel. of F.E.4, 67'9" wings, 2 x R-R [type?] pushers
- F.E.7 variant: long-range heavy bomber, project only

F.E.8 - 1915 single-seat biplane pusher fighter, 295 built
-- F.E.8: 100 hp Gnome Monosoupape 9B rotary engine
-- F.E.8b: [unconfirmed desig.] 110 hp Le Rhône or 110 hp Clerget

F.E.9 - 1917 2-seat recce-fighter, 200 hp HS.8 V8, 3 prototypes built
- F.E.9 first prototype: Apr 1917, single-bay wings (ailerons upper wing only)
- F.E.9 second prototype: Oct 1917, twin-bay wings, trialled by No.78 Sqn
- F.E.9 third prototype: Nov 1917, twin-bay wings, trialled by No.78 Sqn
-- F.E.2 replacement, 24 F.E.9s ordered, cancelled after operational trials
-- led to F.E.12 and N.E.1 night fighter (searchlight and 'rocket gun')

F.E.10 - [Project] B.E.9 devel. as single-seat scout, 200 hp HS.8

F.E.11 - [??] PD Stemp: "Unknown, but possible a lost layout sketch."

F.E.12 - [Project] 1917 2-seat night fighter, 200 hp HS.8 V8, 3 prototypes built
- F.E.12 first prototype: Apr 1917, single-bay wings (ailerons upper wing only)
- F.E.12 second prototype: Oct 1917, twin-bay wings, trialled by No.78 Sqn
- F.E.12 third prototype: Nov 1917, twin-bay wings, trialled by No.78 Sqn
-- Enlarged F.E.9 devel., 24 production ordered (cancelled after op. trials)
-- led to N.E.1 night fighter with searchlight and Vickers 'rocket gun'

H.R.E. Series - Hydroplane Reconnaissance Experimental (See R.E. Below)

H.R.E.1 - R.E.1 floatplane conversion, 70 hp Renault, [unconfirmed]
- H.R.E.1: aka R.E.1 floatplane

H.R.E.2 - floatplane, initial R.E.2 landplane conversion, 100 hp Renault V12
-- Tested from Fleet Pond. After overturning, rebuilt as revised R.E.2 landplane

H.R.E.3 ~ H.R.E.5 - [no evidence]

H.R.E.6 - [Project] 3-seat tractor floatplane, 1 x 250/275 h.p. R-R Falcon engine
- H.R.E.6: aka R.E.6 floatplane

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Royal Aircraft Factory Designations - N.E. and R.E. Series

N.E. Series - Night-flying Experimental

N.E.1 - 1917 2-seat pusher biplane fighter, 1 x 200 hp HS.8, 6 built
-- design begun as F.E.12 (F.E.9 devel.), 3-bay wings, tailbooms, u/c

R.A.M. Series [Non-Existant - Error for 'Ram' names, see A.E. Series above]

R.E. Series - Reconnaissance Experimental

R.E.1 - 1913 recce tractor biplane, 70 hp Renault air-cooled V8
- R.E.1 first prototype: steel-tube fuselage, wing warping (rebuilt w/ ailerons)
- R.E.1 second prototype: longer fuselage, no fin, employed on experimental work
-- Busk made R.E.1 stable (at one point having 4 fins mounted on top of wing)

R.E.2 - 1913 2-seat recce tractor biplane, 70 hp Renault air-cooled V8
-- rebuilt as floatplane H.R.E.2 (qv), 1 x 100 hp Renault V12
- R.E.2 rebuild, ex-H.R.E.2 returned to wheels with new wings and ailerons

R.E.3 - 1913-14 2-seat recce tractor biplane, 120 hp Austro-Daimler
-- R.E.3 airframe identical to H.R.E.2 landplane re-conversion

R.E.4 - [Project] R.E.3 devel. with unequal-span wings, 120 hp Austro-Daimler

R.E.5 - 1914 2-seat recce tractor biplane, 2-bay wings, 120 hp Austro-Daimler
- R.E.5 initial production: equal-span 2-bay wings, unarmed
- R.E.5 later production: some with unequal-span, extended wings, armed
- R.E.5 No. 380: single-seat, long-span wings for high-altitude trials
-- R.E.5 No. 380 - Capt. JHW Becke reached 17,000 ft in June 1914
- R.E.5a: recce-fighter development, redesignated R.E.7 (qv)

R.E.6 - [Project] 3-seat tractor floatplane, 1 x 250/275 h.p. R-R Falcon engine
- R.E.6: aka H.R.E.6

R.E.7 - 1914 2-seat tractor light bomber (orig. envisoned as fighter), 250 built
-- R.E.7 engines: 120 hp Beardmore, RAF 3a or 150 hp RAF 4a, 190 hp R-R Falcon
- R.E.7 3-seater: 160 hp Beardmore, 250 hp R-R Eagle, or 225 hp Sunbeam Maori
-- R.E.7 had extended- unequal span wings similar to high-alt R.E.5 conversion

R.E.8 - 1916 2-seat tractor recce-bomber, 'Harry Tate', 4,077 built, 353 cancelled
- R.E.8 : initial prod'n with pillar-type rear gun mount, later with Scarff ring
-- no desig. change for engine types, 1 x 140 hp RAF 4a or 200 hp RAF 4d
- R.E.8a: 1917 2-bay biplane development of the R.E.8, 250 hp Hispano-Suiza *
- R.E.8: canc. Napier production order (D.4811-D.4885) R-R Eagle [unconfirmed]
- Siddeley R.T.1: enlarged unequal-span 2-bay wings, 3 built (2 with HS, 1 RAF 4a)
- R.E.8: [no desig. change] exp'l inst. of Rateau supercharger on RAF 4d engine
- R.E.8: [no desig. change] unofficial mod., Davis Gun firing through fuse.

[* That '250 hp' Hispano is improbable, 220 hp being tops for the HS.8b and Wolsely Vipers. Flight speculated that the R.E.8a engine may actually have been an "Armstrong Whitworth [sic] Ricardo RHA" ie: the Armstrong-Siddeley Ricardo RHA V12 or Dorman-Ricardo C.I. engine.]

R.E.9 - R.E.8 development (similar to 2-bay R.E.8A), 150 h.p. RAF.4a engine
-- R.E.9 A.3561 tested at Farnborough with Sunbeam Maori

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Royal Aircraft Factory Designations - S.E. and T.E. Series

S.E. Series - Santos Experimental*/Scout Experimental
-- * NB: Santos Experimental applied only to canard configuration

S.E.1 - June 1911 canard pusher biplane, 1 x 59 hp E.N.V Type F V8, x 1
- S.E.1: Type F engine reclaimed from crashed Bleriot XII monoplane

S.E.2 - Oct 1913 single-seat tractor biplane scout, redesignated B.S.2
- S.E.2a: Unofficial desig., Apr 1914 S.E.2 revisions by Henry Folland

S.E.3 - [Project] Apr 1913 high-speed S.E.2 development by Henry Folland
- S.E.3: Development abandoned in favour of more advanced S.E.4 design

S.E.4 - June 1914 high-speed tractor biplane, 1 x 160hp or 100hp Gnome*
-- * Unreliable Gnome 14 Double Lambda replaced by Gnome Monosoupape
- S.E.4: Speed record holder in its day at 135 mph (with Gnome 14)

S.E.4a - 1915 single-seat scout, 1 x 80hp Le Rhône rotary, 4 built
- S.E.4a: To RFC Home Defence sqn but overweight and underpowered

S.E.5 - 1916 single-seat tractor biplane fighter, span 8.11 m
- S.E.5 : Initial prod. model, 1 x 150 hp HS 8a V8, 77 built
- S.E.5a: Improved S.E.5 with geared 200 hp HS 8b or equiv.*
-- * licenced Wolseley W.4A Viper (DD) or W.4B Adder (geared)
- S.E.5b: Refined S.E.5a, 200hp HS 8b, long-span upper wing
-- S.E.5c had streamlined nose & underslung rad, x 1 (A 8947)
- S.E.5E: 1922 US-assembled S.E.5a* from RAF parts, x 56
-- S.E.5E: 1 x 180-hp Wright-Hispano E, aka Eberhart SE-5E
-- * US S.E.5a production by Curtiss orig. planned in 1918

S.E.6 - [Project] Single-seat scout biplane, 1 x RR Falcon or R.A.F. 4d
-- NB: P.D. Stemp lists as R.A.F. 6

S.E.7 - [Project] radial-engined R.A.F.6, poss. 1 x RAF 8 14-cyl
-- NB: P.D. Stemp lists as RAF 7

T.E. Series - Tatin Experimental

T.E. -- [Project] 1917 monoplane, pusher prop (behind tail)

T.E.1 - [Project] 2-seat fighter based on scaled-up S.E.5
- T.E.1: 6 prototypes planned (A 8951 - A 8956), unbuilt
-- 1 x 200hp HS.8, 31'3" span, 1 x Vickers/1x Lewis gun

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Royal Aircraft Factory Designations - RAF Engines

RAF 1 -- 1913 liquid-cooled V8 (enlarged French Renault 70/80 hp) 540 cid (8.8 L)
- RAF 1: January 1913 and delivering 100 hp
- RAF 1a increased bore: 1915, 590 cid (9.7 L), 115 hp at 1,800 rpm.
- RAF 1a supercharged: late 1915 experimental version (test flown in B.E.2c)
-- geared, single-stage supercharger, trial intallation by James Ellor

RAF 2 -- 1913 air-cooled, 9-cyl radial engine, 120 hp, design by F.M. Green (Oct 1913)
-- RAF 2 had the same bore and stroke as the RAF 1, test engine, 605 cid (9.9 L)

RAF 3 -- liquid-cooled V12 (based on RAF 1) built Armstrong Whitworth and Napier
- RAF 3 : 1914 prototype engine, 200 hp
- RAF 3a: 1914 prod. version, 260 hp (via increased bore), 1050 cid (17.24 L)
-- Armstrong Whitworth built 29 RAF 3a engines
-- Napier & Son built 260 RAF 3a engines

RAF 4 -- 1915 liquid-cooled V12 (actually design by AJ Rowledge at Napiers)
-- V12 based on Napier-built RAF 3 but intended to RAF 1a components
- RAF 4 : 1914-15 prototype design aimed at 150 hp (acheived 140 hp)
- RAF 4a: 1916 refined design with 2 x gear oil pump, flywheel omitted
-- RAF 4a production engine acheived 160 hp, 3,608 built
- RAF 4b: [??]
- RAF 4c: RAF 4a development with aluminium side-valve cylinders
- RAF 4d: 1916 aluminium cyl. liners and pistons repl. steel, output 220 hp
- RAF 4d with experimental Rateau supercharger, 16 built (eg: R.E.8 B738)
- RAF 4e: 1917 devel., strengthened cylinders, enlarged valves, 240 hp
-- The supercharged RAF 4e was to be fitted to the R.E.8
- RAF 4? : [Project] late 1917 Ellor-Metrovick turbo-supercharger of RAF 4

RAF 5 -- 1915 liquid-cooled V12, pusher variant of RAF 4
- RAF 5 : 1915 150 hp fan-cooled pusher variant
- RAF 5b: 19[??] enlarged bore version of RAF 5, 170 hp

RAF 6 -- [??]

RAF 7 -- V12, high compression version of the RAF 3a (high-lift camshafts)

RAF 8 -- Unbuilt 14-cyl air-cooled radial engine design by F. M. Green
- RAF 8: Evolved into Siddeley Deasy/Armstrong Siddeley Jaguar engine

RAF 9 -- [??]

RAF 10 - [Project] design study for liquid-cooled V12 (based on Hispano engines)

_______________________

Note: The Royal Aircraft Factory applied 'RAF 27T' to a for a 1918 patent by James E. Ellor for a turbocharged 2-stroke 6-cyl rotary engine. It is not clear whether this was an official type designation or simply applied as a drawing number. If so, RAF 11 through RAF 26 engine designations remain to be uncovered!

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Amazing a prefect work my dears Apophenia and AM,and I can add;


B.E.11 someone suggested that,it was anther variant of B.E.2 .


Hurricane was single seat mid-wing ultra-light monoplane of 1923,powered by one
600 cc engine.


Zephyr was single seat twin boom ultra-light biplane,powered by one 500 cc engine.


Scarab was single seat parasol-wing light monoplane,powered by one 32 hp
Bristol Cherub III engine.


Sirocco was single seat ultra-light monoplane,powered by one 32 hp Bristol Cherub III
engine,never completed.


Rafwire experimental aircraft,no more details.
 
Thanks folks!

Hesham: Thanks for the B.E.11 connection. RAFwires (or rafwire) were streamlined, high-tensile bracing wires (as used on the S.E.5a).

Hurricane, Zephyr, and Scarab were designed and built the Royal Aircraft Establishment's Aero Club -- the R.A.F. being renamed R.A.E. in 1918. Below is a separate list of RAE design names.

Royal Aircraft Establishment/RAE Aero Club Aircraft Design Names

RAE Target — 1922 R/C monoplane surface-to-surface missile, 23 ft span
- Target: Catapulted from HMS Argus (Aug 1922) HMS Stronghold (Sept 1924)

RAE Hurricane - 1923 single-seat light monoplane*, span 7.01 m, x 1
- Hurricane: designed for the 1923 Lympne Motor Glider Competition
-- * Shoulder-mounted wing on a triangular-sectioned fuselage
-- 1923 21.5 hp Douglas HO 2-cyl, 1924 32 hp Bristol Cherub II

RAE Zephyr - 1923 single-seat pusher light biplane, span 7.01 m, x 1
- Zephyr: designed for the 1923 Lympne Motor Glider Competition
-- 1923 17 hp Douglas HO 2-cyl, x 1 (G-EBGW)

RAE Larynx — 1927 R/C monoplane SSM 'flying torpedo' (250 lb warhead)
- LARYNX = Long Range Gun with Lynx engine, same guidance system as RAF AT
-- 200 hp Armstrong Siddeley Lynx IV, 250 lbs HE, range 300 miles+
-- http://www.flightglobal.com/pdfarchive/view/1958/1958%20-%200642.html

RAE Scarab - 1932 single-seat parasol light monoplane, span 9.14 m
- Scarab: DH.53 wings/empennage on a new fuselage, x 1 (G-ABOH)
-- 1 x 32 hp Bristol Cherub III HO 2-cyl air-cooled engine
 

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