Gourdou-Leseurre GL.30

__NOTOC__ Infobox Aircraft
name=GL.30


caption=
type=Fighter
national origin=France
manufacturer=Gourdou-Leseurre
designer=
first flight=avyear|1920
introduced=
retired=
status=
primary user="Aéronautique Militaire"
more users="Aéronautique Maritime"
produced=
number built= >500
variants with their own articles=The Gourdou-Leseurre GL.30 was a racing aircraft built in France in 1920 which formed the basis for a highly-successful family of fighter aircraft based on the same design. The GL-30 was a parasol-wing monoplane with retractable undercarriage and a Bristol Jupiter engine. In 1922, this was used to develop a fighter under the designation GL.31. Generally similar to its predecessor, the GL.31 had a greater wingspan, fixed undercarriage, a Gnome-Rhône 9A engine, and was armed with four machine guns; two in the forward fuselage and two in the wings. While this remained a development aircraft, it paved the way for the company's entry in a forthcoming "Aéronautique Militaire" competition to select a new fighter, announced in 1923.

By the time the prototype flew, the Gourdou-Leseurre had been acquired by Loire, and therefore the new aircraft was entered as the LGL.32. Placed second in the trials, the type's performance was impressive enough to still result in an order in January 1927 for a small batch of aircraft - five evaluation aircraft and 20 pre-production machines. Eventually, 475 of this basic version, dubbed LGL.32C.1 in service, would be ordered by the "Aéronautique Militaire" and 15 more by the "Aéronautique Maritime". Romania ordered a further 50 aircraft of the same design as the examples in French service, Turkey ordered 12 (these designated LGL.32-T) and another one may have been purchased by Japan.

In French service, development turned from fighters to adapting the aircraft as a carrier-borne dive bomber. These featured general strengthening of the airframe, divided main undercarriage units, and a "fork" under the fuselage able to release a 50 kg (110 lb) bomb from under the fuselage while avoiding hitting the propeller.

While prolific, the GL.32 was not long-lasting, and attrition took a heavy toll on them. By 1934, all remaining examples were relegated to training and as instructional airframes; at the start of 1936, only 135 remained of the original 380 purchased. A number of these were sold to the government of the Second Spanish Republic and to the Basque Nationalist Party. Another aircraft was supplied to the Basques in 1937, modified as a dive-bomber along the lines of the previous French experiments. Designated the GL.633, this aircraft was used by Miguel Zambudio to attack the Nationalist battleship "España", scoring decisive hits that contributed substantially to her subsequent sinking.

Variants

GL.30

* GL.30 - Racer with retractable undercarriage and Bristol Jupiter engine (1 built)
* GL.31 - Four-gun fighter prototype with fixed undercarriage, longer-span wings and Gnome-Rhône 9A engine (1 built). Also known as the GL.31C.1 or CL-I-3.
* LGL.32 - Definitive two-gun fighter version (ca. 490 built). Also known as the GL.32C.1.
** LGL.32.01 - The first prototype.
** LGL.32T - Export version for Turkey (12 built)
** LGL.32 Hy - Twin-pontoon floatplane version converted from LGL.32 prototype. Set world seaplane altitude record on 28 March 1927 (1 converted)
** LGL.321 - LGL.32 converted to use 450 kW (600 hp) version of Bristol Jupiter (1 converted)
** LGL.323 - LGL.32 converted to use supercharged 373 kW (600 hp) Bristol Jupiter for unsuccessful altitude record attempts. (1 converted)
** LGL.324 - LGL.323 further modified and used by Pierre Lemoigne to set world landplane altitude record with 500 kg payload of 9,600 m (31,500 ft) on 23 May 1929 and Albert Lécrivain to set world landplane altitude record of 11,000 m (39,090 ft) on 24 October. (1 converted)
* LGL.33 - Similar to LGL.32 but with Lorraine 12Eb engine, and revised wing struts, landing gear, and tail (1 built). Also known as the LGL.33C.1.
* LGL.34 - Similar to LGL.32 but with Hispano-Suiza 12Gb engine (1 built). Also known as the LGL.34C.1.
** LGL.341 - similar to LGL.32 with Hispano-Suiza 12Hb engine (2 built, second with revised radiator arrangement)
* LGL.35
** LGL.351 - version with Renault 12J engine (1 built)
* LGL.390 - night fighter prototype with Hispano-Suiza 9Va engine (1 converted from LGL.32)

GL.40

* GL.410 - modernised fighter with divided main undercarriage (1 built)
* GL.430 - strengthened carrier-borne dive-bomber prototype (1 built)
** GL.432 - dive-bomber variant similar to GL.430 used for operational testing (4 built)
* GL.450 - fighter version
* GL.480
** GL-482 - fighter version with Hispano-Suiza 12Xbrs engine (1 built)

GL.520

* GL.520
** GL.521 - dive-bomber version with Gnome-Rhône 9Kfr engine and taller tail fin (2 built)

GL.60

* GL.630
** GL.633 - dive-bomber similar to GL.432 (1 built)

Operators

;FRA
*French Air Force
*French Navy;ROM;flag|Spain|1931
*Spanish Republican Air Force;;flag|Basque Country
*Basque Nationalist Party;TUR

pecifications (LGL-32C.1)

aerospecs
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met or eng?= met

crew=One, pilot
capacity=
length m=7.55
length ft=24
length in=10
span m=12.20
span ft=40
span in=0
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
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width m=
width ft=
width in=
height m=2.95
height ft=9
height in=8
wing area sqm=24.9
wing area sqft=268
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=963
empty weight lb=2,123
gross weight kg=1,376
gross weight lb=3,033
lift kg=
lift lb=

eng1 number=1
eng1 type=Gnome-Rhône 9Ady
eng1 kw= 313
eng1 hp= 420
eng1 kn=
eng1 lbf=
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eng2 number=
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max speed kmh=250
max speed mph=155
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=500
range miles=311
endurance h=
endurance min=
ceiling m=9,700
ceiling ft=31,800
glide ratio=
climb rate ms=6.9
climb rate ftmin=1,370
sink rate ms=
sink rate ftmin=

armament1=2 × fixed, forward-firing .303 Vickers machine guns
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armament6= aircontent
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References

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