Simplex Aircraft Corp S-2 Kite / Sioux Kite

A monoplane called the S-2 Kite was developed in 1931. Designed by Omer Woodson, it was a probe into the inexpensive, ultralight aircraft market.

It had an uncovered, girder-like fuselage, and thick, cantilever wing. One was built, NX489M c/n 1002.

Simplex failed to get anywhere with the project, but the idea went with Woodson and company test pilot Myhres when they left in 1930 to form Cycloplane Co.

Sioux Aircraft Corporation built aircraft under the name Sioux Kite.

S-2 Kite
Engine: Szekely SR-3, 40hp
Seats: 1

Simplex Aircraft Corp K-2 Red Arrow

Simplex K-2-C

The 1928 Simplex K-2-C Red Arrow (ATC 44) was designed by Omer Woodson with origins in the Woodson M-6. Of wooden construction it was Side-by-side canopied cockpit and semi-cantilever wing. The first few were powered by 75hp Kinner engines and priced at $4,495.

The 1928 Simplex K-2-S Red Arrow (ATC 43) was the same as the K-2-C, but with side-by-side open cockpit and priced at $4,115.

Simplex K-2-S

About 10 K-2s were built. Piloted by Dick Myhres, one, NC6504, won the 1928 California Class-A Race (Los Angeles-San Francisco) in a field of 16 aircraft in 3hr10min averaging 126mph.

Sioux Aircraft Corporation built aircraft under the name Sioux Red Arrow.

K-2-C Red Arrow
Engine: 90hp Kinner K-5
Wingspan: 34’4″
Length: 22’3″
Useful load: 570 lb
Max speed: 120 mph
Cruise: 108 mph
Stall: 37 mph
Range: 550 mi
Seats: 2

K-2-S Red Arrow
Engine: 90hp Kinner K-5
Wingspan: 34’4″
Length: 22’3″
Seats: 2

Simplex Racer

The first design of the Simplex firm was a racing monoplane with a 320 hp Hispano-Suiza engine for the Coupe-Deutsch race of 1922. The design was due to Carmier, and the plane was to be flown by a well-known fighter pilot, Georges Madon. It was a cantilever monoplane with a tractor engine and full-span controllers. The short fuselage ended in a vertical fin with a rudder. The pilot sat rather far back behind the leading edge of the wing ; in addition, a barrel radiator excluded any view forward. So it was not surprising that even a very experienced pilot like Madon could meet with an accident during a test flight prior to the race. He escaped with severe injuries, and the general impression created was rather unfortunate. Since Fétu had previously met with a grave accident with the Arnoux biplane, the fate of this interesting development was sealed. Arnoux himself seems to have been discouraged from further pursuing his line of investigation.

Simonini Victor

Victor 2

Circa 1998, fits on Rotax 582 engine mount.

Victor 2

Simonini Victor 2 Engine 92 HP (Victor 2) or 103 HP (Victor 2 Plus)
Twin Cylinder, 2-Stroke
Water Cooled
Dual ignition
Dual Carburettors
Prop drive via reduction drive
Fits on Rotax 582 engine mount.

Victor 2
Cycle: 2 stroke
No cylinders: 2 inline
Bore: 78 mm
Stroke: 72 mm
Compression: 10
Displacement: 688 cc
Cooling: Liquid
Ignition: DCDI
Reduction: 2.76-4/1
Weight: 55 kg
Max pwr: 92 hp at 6100 rpm
Max torque: 10.8 kgm @ 5900 rpm
Fuel consumption: 9.5 lt/hr @ 5000 rpm
Price 1998: 9500 DM

Simmonds Spartan Cruiser

Cruiser III G-ADEM – 8 March 1936

Spartan Cruiser was development of Saro-Percival (later Spartan) Mailplane G-ABLI of 1931. After
Percival sold his interest to Saunders-Roe Ltd, which eventuaally tied up with Spartan, the concept under the Spartan name into the Spartan Cruiser I, powered by three 120 hp de Havilland engines and carrying six passengers and two crew in a metal fuselage.

Spartan Cruiser c/n 2 YI-AAA

Early production Spartan Cruiser c/n 2 was operated by Airwork (Iraq) Ltd in 1933 on an air route between Baghdad and Mosul as YI-AAA. It returned to the UK in 1934 for British Airways Ltd and reverted to its original registration of G-ACBM. It was scrapped in 1937.

Spartan Cruiser c/n 2 YI-AAA

Twelve Spartan Cruiser II were built.

Three Cruiser III were built. The last was G-ADEM in May 1935.

Specifications:

Cruiser I
Engines: 3 x de Havilland, 120 hp

Cruiser II

Cruiser II
Engines: 3 x de Havilland Gipsy Major, 130 hp