Savoia-Marchetti heavy fighter prototypes

The Savoia-Marchetti SM.88, SM.91 and SM.92 were Italian twin-engined heavy fighter prototypes of World War II. All featured a dual-fuselage structure and used German Daimler-Benz engines.

Savoia-Marchetti SM.88

SM.88
Type	Heavy fighter
Manufacturer	Savoia-Marchetti
Maiden flight	1939
Number built	1

The SM.88 was created around 1938 and intended for export. Resembling the P-61 Black Widow, it was a light-medium, land based, multi-role fighter. This was a new concept for Italian aircraft industries, though Savoia had already developed a similar aircraft with the S.55, which had twin fuselages without a central nacelle. The SM.88 was meant as an advanced combat aircraft, offering modern design at low cost.

The SM.88 had a crew of three; two pilots and a rear gunner. The crew nacelle was located in the middle of the wing structure linking the two fuselages, behind the two Daimler-Benz DB 601 engines. The cockpit was entirely glassed and the upper part could be ejected.

The tail had two vertical rudders with a single horizontal surface between. The retractable landing gear consisted of four wheels, two in the front and back, respectively. The structure was a wooden frame covered with a metal skin.

When the aircraft bombed a target, the pilot took on the role of bombardier. To improve accuracy the pilot lay on the floor of the fuselage while the co-pilot flew the aircraft. The rear gun was encased in a flexible plastic enclosure in the rear fuselage while two more 12.7 mm Breda-SAFAT machine guns were fixed in the wings.

The aerodynamic design of the plane gave it good performance at a low cost and it was presented for consideration to Regia Aeronautica in 1939. However with the coming of World War II the export of Italian aircraft with DB601 engines was forbidden.

Unfortunately for Savoia-Marchetti, the Messerschmitt Bf 110, with the same engines, was almost as fast as the SM.88, but featured a much more conventional and reliable layout (and better armament). Thus only one prototype SM.88 was built.

In 1942, Regia Aeronautica requested a redesign of the aircraft into a fast reconnaissance aircraft or bomber. They requested a range of 2,000 km (1,240 mi) with auxiliary tanks, or 1,500 km (930 mi) with 500 kg (1,100 lb) bombload (with an effective radius of 750 km (465 mi)).

Specifications (SM.88)

General characteristics

• Crew: Three; pilot, co-pilot, rear-gunner
• Length: 12.1 m (39 ft 8 in)
• Wingspan: 14.5 m (47 ft 6 in)
• Height: 3.5 m (10 ft 6 in)
• Wing area: 32.5 m² (349.7 ft²)
• Empty weight: 5,000 kg (11,000 lb)
• Loaded weight: 7,000 kg (15,400 lb)
• Powerplant: 2× Daimler-Benz DB 601 liquid-cooled supercharged inverted V12 engines, () each
• Fuel: 1,250 litres in 10 wing tanks

Performance

• Maximum speed: 560 km/h (302 knots, 348 mph)
• Service ceiling: 8,700 m (28,535 ft)
• Climb to 5,000 m (16,400 ft): 12 min. 30 sec.

Armament

3 × 12.7 mm Breda-SAFAT machine guns

600 kg (1,320 lb) bombload

Savoia-Marchetti SM.91

SM.91
275px
Type	Fighter/bomber
Manufacturer	Savoia-Marchetti
Maiden flight	11 March 1943
Number built	2

Savoia-Marchetti first developed the SM.91, a long range fighter/bomber, to compete in a contract offered by the Regia Aeronautica to the Italian aircraft companies in 1938.

In July 1942, the Regia Aeronautica requested designs for a new aircraft, propelled by the DB605 engine, capable of flying at 620 km/h (385 mph) with a range of 1,600 km (995 mi). The armament should consist of six MG 151 cannon in the nose and wings and a 12.7 mm Breda-SAFAT machine gun as a defensive weapon. It should have a 800 kg (1,760 lb) bombload. At this point, the request for a long range fighter killed the SM.88, still in development, and the SM.91, a larger, heavier and more modern design, was authorized.

The fuselage and the wings were all-metal, to achieve the best performance regardless of cost. The central nacelle held the crew of two, and the wings and tail was similar to the SM.88. Fuel capacity was 1,600 liters. but with auxiliary tanks could be raised to 1,800 liters. It is unknown if it was capable of a range of 1,600 km.

The two DB 605 engines gave a total of 2,950 hp. The aircraft's maximum speed at 585 km/h (363 mph), was better than the SM.88. There were three 20 mm MG 151 cannon in the nose. Two more were mounted in the wings, close to the fuselage. Another machine gun was provided for the rear gunner. Total bombload was 1,640 kg (3,608 lb) or a torpedo.

The prototype, designated MM.530, flew for the first time on 11 March 1943, tested by Aldo Moggi. There were two prototypes, the second a modified SM.88 prototype.

The machine flew at Vergiate and logged 27 hours in the next few months. It was advanced, but was not entered into the official tests at Guidonia, perhaps because it was still undergoing testing. The first prototype was captured and sent to Germany in October 1943, after which it vanished and is presumed destroyed. The second prototype was captured by the Germans incomplete when they occupied northern Italy in September 1943. This aircraft was tested on 10 July 1944, but was destroyed by Allied bombers later in the year.

Specifications (SM.91)

General characteristics

• Crew: Two, pilot and rear gunner
• Length: 13.25 m (43 ft 6 in)
• Wingspan: 19.7 m (64 ft 7 in)
• Height: 3.85 m (12 ft 7 in)
• Wing area: 41.76 m² (449.3 ft²)
• Empty weight: 6,400 kg (14,080 lb)
• Powerplant: 2× Daimler-Benz DB 605 liquid-cooled supercharged inverted V12 engines, () each

Performance

• Maximum speed: 585 km/h (315 knots, 363 mph)
• Range: 1,600 km (864 nm, 995 mi)
• Service ceiling: 10,800 m (35,425 ft)
• Climb to 6,000 m (19,680 ft): 7 min. 40 sec.

Armament

5 × 20 mm MG 151 cannons

1,640 kg bombload

Savoia-Marchetti SM.92

SM.92
275px
Type	Heavy fighter
Manufacturer	Savoia-Marchetti
Maiden flight	October 1943
Number built	1

Another heavy fighter/bomber based on the SM.88 was the SM.92. The SM.92 did away with the mid-wing crew nacelle. The crew of two sat in the left fuselage only. Two DB 605 engines were fitted.

Armament consisted of three 20 mm MG 151 cannon, two in the mid-wing and one in the right fuselage, and three 12.7 mm machine guns, one under each engine, and one remotely-controlled in the tail. A bombload of up to 2,000 kg (4,400 lb) could be carried under the inner wing, and 160 kg (350 lb) bombs were carried under the outer wings.

The maximum speed was increased, but still did not meet that required. It had a complex and advanced structure which contributed to difficulties in producing a working prototype. The prototype MM.531 flew for the first time in October 1943 and logged over 21 hours of flight time. In March 1944 it was mistaken for a P-38 Lightning and attacked by a Macchi C.205. The aircraft survived by performing evasive manoeuvres, but it was so badly damaged that it was grounded for months. The SM.92 was destroyed by Allied bombing in 1944.

Specifications (SM.92)

File:Sm92 rear.jpg

SM.92 rear view

General characteristics

• Crew: Two, pilot and rear gunner
• Length: 13.7 m (44 ft 11 in)
• Wingspan: 18.55 m (60 ft 10 in)
• Height: 4.15 m (13 ft 7 in)
• Wing area: 38.52 m² (414.5 ft²)
• Empty weight: 5,900 kg (12,980 lb)
• Powerplant: 2× Daimler-Benz DB 605 liquid-cooled supercharged inverted V12 engines, () each

Performance

• Maximum speed: 615 km/h (332 knots, 382 mph) at 6,700 m (21,976 ft)
• Range: 2,000 km (1,080 nm, 1,243 mi)
• Service ceiling: 12,000 m (39,360 ft)
• Climb to 6,000 m (19,680 ft): 7 min. 10 sec.

Armament

3 × 20 mm MG 151 cannons

3 × 12.7 mm Breda-SAFAT machine guns

Up to 2,000 kg (4,400 lb) bombload

See also

Related lists

• List of aircraft of Italy, World War II

References

• Lembo, Daniele, I bifusoliera della Regia, Storia militare magazine, Westward editions, n.11, April-May 2000 Template:It icon

External links

• SM.91 & SM.92

This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Savoia-Marchetti heavy fighter prototypes".