 
         
           
         
         In July 1934 Avions 
         Mareel Bloch was a contender in a design competition which resulted 
         from a French air ministry specification for a new fighter. Submissions 
         were received also from Dewoitine, Loire, Morane-Saulnier and Nieuport, 
         with Morane-Saulnier eventually selected as the winner. So far as Bloch 
         was concerned, this was no close-drawn decision with its design team 
         chewing its finger nails because it had been beaten to the pylon by the 
         thickness of the paint skin on the propeller. True, it was biting its 
         finger nails; but this was probably because its Bloch M.B.150.01 
         prototype could not be induced to part company with the security of 
         mother earth. 
         Nothing further 
         happened for about nine months until, in early 1937, it was decided to 
         force the 'ugly duckling' into the air. This was achieved in October 
         1937 after the provision of a strengthened wing of greater area, 
         revised landing gear, and installation of a 701 kW (940 hp) Gnome-Rhone 
         14No radial engine with a three-blade constant speed propeller. Handed 
         over to the Centre d'Essais du Materiel Aerien (CEMA) for service 
         trials, its performance proved sufficiently interesting to warrant 
         further development. This brought, at the very beginning of 1938, a 
         small increase in wing span and installation of a Gnome-Rhone 14N-7 
         engine. When trials were completed in the late spring of 1938, SNCASO 
         was awarded an order for a pre-production batch of 25 of these 
         aircraft. 
         Preparatory work before 
         initiation of construction of the aircraft, in a new SNCASO factory, 
         brought realisation thatdesignoftheM.B.150.Ol was totally unsuited for 
         mass production. The only solution was another redesign, during which 
         wing area was reduced and the Gnome-Rh6ne 14N-11 engine selected for 
         installation. It was in this form that a new prototype, redesignated 
         M.B.151.01, flew for the first time on 18 August 1938. Construction of 
         the balance of the pre-production order had already started by then, 
         but despite the growing urgency of the situation only four of these 
         aircraft had been delivered by April 1939. Simultaneously, SNCASO's 
         design team had been working on an improved version, but the only 
         significant difference between this and the M.B.151.01 lay in the 
         installation of a 768 kW (1,030 hp) Gnome-Rhone 14N-21 engine. First 
         flown in December 1938 the new prototype, designated M.B.152.01, was 
         provided with the slightly more powerful Gnome-Rhone 14N-25 before 
         being handed over to the CEMA for flight testing in February 1939. The 
         improved performance of this version created positive reaction, with a 
         firm order being placed for 400 production aircraft, of which 340 were 
         to be M.13.152s, the balance the earlier M.B.151s. 
         
           
         Three view diagram of the Block MB-152 
         Unfortunately, equally 
         positive action did not materialise on the production line, and by the 
         out-break of World War 11 in September 1939 a combined total of 120 
         M.B.151 and M.B.152s had been delivered. Even more unfortunately, not 
         one of these could be used in action, for all were without gunsights 
         and 95 of them could not be used at all, for they had been delivered 
         without propellers. This was the moment when pressure of circumstances 
         should have eliminated all petty difficulties, but even by the end of 
         November, at which time 358 had been delivered, 157 were still without 
         propellers and there were serious problems with engine overheating 
         which needed attention. 
         Despite the problems, 
         the Armee de I'Air did everything possible to speed introduction of 
         what was potentially a valuable addition to its inventory. An 
         experimental squadron was formed in September 1939, and initial 
         deliveries to the fighter groupes began in the following month. Initial 
         unit to convert to the type was Groupe de Chasse Ill, and by the end of 
         1939 newly equipped groupes included II/1 and II/10, III/9 and III/10, 
         and the French Navy's Escadrille AC-3. All were to discover that their 
         M.B.151s and M.B.152s possessed the desirable attributes of a combat 
         aircraft, and it was tragic that indifference and political intrigue 
         forced so many courageous pilots of the Armee de I'Air to lose their 
         lives in obsolete aircraft, instead of being able to contest the 
         Luftwaffe on more equal terms with fighters such as the M.B.152. 
         When the German 
         armoured Divisions swept through France in May 1940, Groupes I/8, II/8 
         and II/9 had also been equipped with these fighters and, just before 
         this, nine M.B.151s had been supplied to the Greek air force. After the 
         collapse of France and conclusion of the Franco-German Armistice, six 
         groupes of the Vichy French air force retained M.B.151 and M.B.152 
         aircraft, namely I/l and I/8, II/1, II/8 and II/9, III/9, and when 
         SNCASO production ended at the same time a total of more than 600 had 
         been built. When, subsequently, three of these groupes were re-equipped 
         with Dewoitine fighters, the M.B.151s and M.B.152s were handed over to 
         the Romanian air force. 
         The only variant 
         comprised one M.B.153.01 prototype, an M.B.152 taken from the 
         production line and re-engined with a 783 kW (1,050 hp) Pratt & Whitney 
         R-1830-SC3-G Twin Wasp engine. 
         Specifications (Bloch 
         MB-152) 
         Type: Single 
         Seat Fighter 
         Design: Marcel 
         Bloch  
         Manufacturer: 
         SNCASO  
         Powerplant: One 
         1,080 hp (805 kw) Gnome-Rhone 14N-25 or a 1,100 hp (820 kw) 14N-49 
         14-cylinder radial piston engine. 
         Performance: 
         Maximum speed 320 mph (515 km/h) at 13,125 ft (4000 m); maximum 
         cruising speed 280 mph (450 km/h); service ceiling 32,810 ft (10000 m). 
         Range: 373 miles 
         (600 km) with internal fuel stores. 
         Weight: Empty 
         4,453 lbs (2020 kg) with a maximum take-off weight of 5,908 lbs (2680 
         kg). 
         Dimensions: Span 
         34 ft 7 1/4 in (10.55 m); length 29 ft 10 1/4 in (9.10 m); height 12 ft 
         11 1/2 in (3.95 m); wing area 161.46 sq ft (15.00 sq m). 
         Armament: Two 20 
         mm Hispano 404 cannon (60 round drum each), and two 7.5 mm (0.295 in) 
         MAC 1934 machine guns (500 rounds each) or four 7.5 mm (0.295 in) MAC 
         1934 machine guns. 
         Variants: MB-150 
         (first prototype, but it was such a bad aircraft, it never flew), 
         MB-151 (much improved MB-150 redesign with a Gnome-Rhone 14N-11 
         engine), MB-152 (upgraded engine), MB-153-01 (a stock MB-152 with an 
         American engine).  
         Operators: 
         France (Armee de l'Air, Vichy AF), Greece, Romania. 
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