Moskalyev SAM-14

Last updated
SAM-14
Moskalev SAM-14.jpg
RoleUtility transport
National origin USSR
ManufacturerGAZ-18,Voronezh
DesignerAleksandr Sergeyevitch Moskalyev
First flight1939

The Moskalyev SAM-14 was a late 1930s Soviet, five-passenger transport, one of a series of developments of the successful Moskalyev SAM-5.

Contents

Design and development

The single engine, high wing Moskalyev SAM-5bis-2 was a 1934 light transport developed into four different types, of which the SAM-14 was the penultimate. Apart from having a more powerful, inline engine, it was similar to the original. [1]

It had the same high-set two spar, cantilever wing as the SAM-5bis-2, with ply-skin ahead of the forward spar forming a torsion resistant box. The whole surface, including the ply-skinned leading edge, was fabric covered. The SAM-14's wings had Kalman flaps [ clarification needed ]. [1]

It was powered by a nose-mounted 110 kW (150 hp) Voronezh MV-4 4-cylinder, air-cooled, inverted inline, a licence-built Renault 4Pei engine. The fuselage had a wooden girder structure and was plywood-covered forward of the rear of the cabin, under the trailing edge, and fabric covered aft. The pilot's enclosed cockpit was ahead of the wing leading edge and its five-place passenger cabin was behind him under the wing, with three windows on each side and two port side doors. Behind the cabin the fuselage was fabric covered, narrowing to the SAM-5bis-2-style tail, with a blunted triangular fin and more rounded rudder. A triangular plan tailplane was mounted on top of the fuselage and carried rounded, tabbed elevators, separated for rudder movement. [1]

The SAM-14 had wide-splayed cantilever landing gear, each side with a landing leg and drag strut within a common fairing. The few photographs show it on short main skis and a tail ski. [1]

Operational history

The date of the SAM-14's first flight is not known but official testing began in November 1939 and continued until June 1940. Production was initially approved but then cancelled by higher authority. [1]

Specifications

Data from The Osprey Encyclopedia of Russian Aircraft 1875-1995 [1]

General characteristics

Performance

Related Research Articles

Potez 661

The Potez 661 was a four-engined metal low-wing monoplane airliner developed in France just before World War II. The single example flew with Air Afrique on French colonial routes.

CANT Z.1012

The CANT Z.1012 was a small three-engined monoplane built in Italy in the late 1930s to carry either three or five passengers depending on the engines. A small number were built for Italian diplomatic use.

Praga E-210

The Praga E-210 was a four-seat, twin-engined touring aircraft built in Czechoslovakia in the late 1930s. It had an unusual pusher configuration. Its tail unit and undercarriage were modified significantly before World War II and after the war a more powerful version designated E-211 was flown.

The Johansen CAJO 59 was a Danish twin-engined amphibious flying boat. Built in the late 1960s, it achieved certification but did not go into production.

The Moskalyev SAM-25 was an early 1940s Soviet, military assault transport, the last of a series of developments of the successful Moskalyev SAM-5.

SNCASE SE-2100

The Sud-Est or SNCASE SE-2100, sometimes known as the Satre SE-2100 after its designer, was a tailless, pusher configuration touring monoplane with a single engine and cabin for two. Only one was built.

SNCASE SE-2300

The Sud-Est SE-2300 or S.N.C.A.S.E. SE-2300 was a two/three seat low wing, single engine touring aircraft, built just after World War II in France. The SE-2310 was a tricycle undercarriage variant. Neither type went into production.

Gribovsky G-22

The Gribovsky G-22 was a low powered, single seat sports cantilever monoplane, designed and built in the USSR in the mid-1930s. It set at least one class record and flew from 1936 to at least 1940, though only one was completed.

The Gribovsky G-28 was an advanced trainer for trainee fighter pilots, built in the USSR just before the German invasion in 1941. It satisfied VVS testing but changing priorities led to the abandonment of production plans.

Caudron C.430 Rafale

The Caudron C.430 Rafale was a fast, two seat French touring monoplane. Soon after its first flight in 1933 it set an international class speed record.

The Caudron C.580 was a French advanced trainer aircraft intended to prepare pilots for the new low wing monoplane fighters of the mid-1930s. It did not go into production and only two were built.

The Caudron C.570 was a French twin-engine aircraft designed and built by Caudron in the mid-1930s. It was designed to function in multiple roles; as a bomber, passenger transport, paratroop aircraft, cargo aircraft and air ambulance.

Morane-Saulnier MS.350

The Morane-Saulnier MS.350 was a French aerobatic trainer flown in 1936. Only one was built but it had a long career, flying post-war until the 1960s.

The Möller Stomo 3 was a small, low-powered but very aerodynamically-clean light aircraft, first flown in Germany in 1939. It set two speed over distance records for aircraft with engines of less than 2 l (120 cu in) capacity soon after its first flight.

The WNF Wn 16 was an Austrian experimental aircraft built near the start of World War II to test the properties of the then-new tricycle undercarriage arrangement.

The Bodiansky 20, a French four-seat touring aircraft flown in the early 1930s, was one of the first French aircraft to adopt Handley Page slots to delay the stall and lower landing speed.

Moskalyev SAM-9 Strela

The Moskalyev SAM-9 Strela (Arrow) was a one-off, Soviet, 1930s experimental tailless aircraft designed to test the characteristics of an ogival delta wing.

The Moskalyev SAM-10 was a late 1930s Soviet light transport aircraft suited to passenger or ambulance roles. Despite proving outstanding in trials, engine supply curtailed its production.

The Moskalyev SAM-11 was an amphibious version of the SAM-5bis-2, with a flying boat hull, retractable landing gear and raised engine and tail to avoid spray. Only one was built.

Ogden Osprey

The Ogden Osprey was a three engine, high wing monoplane airliner which seated six. Designed in the United States and first flown in the spring of 1930 or earlier, six were built and some used commercially before Ogden Aeronautical ceased trading in the Great Depression.

References

  1. 1 2 3 4 5 6 Gunston, Bill (1995). The Osprey Encyclopedia of Russian Aircraft 1875-1995. London: Osprey (Reed Consumer Books Ltd). p. XXI, 253. ISBN   1-85532-405-9.