1929
Engine: 1 x 300hp Armstrong Siddeley Cheetah IV
Wingspan: 12.40 m / 41 ft 8 in
Length: 8.00 m / 26 ft 3 in
Height: 3.40 m / 11 ft 2 in
Wing area: 34.00 sq.m / 365.97 sq ft
Max take-off weight: 1380 kg / 3042 lb
Empty weight: 960 kg / 2116 lb
Max. speed: 205 km/h / 127 mph
Cruise speed: 185 km/h / 115 mph
Crew: 2
1924
Engine: 1 x 300hp Hispano Suiza
Wingspan: 14.30 m / 47 ft 11 in
Length: 8.80 m / 29 ft 10 in
Height: 4.20 m / 14 ft 9 in
Max take-off weight: 1640 kg / 3616 lb
Empty weight: 1120 kg / 2469 lb
Max. speed: 200 km/h / 124 mph
Cruise speed: 180 km/h / 112 mph
Crew: 2
A monoplane built in Argentina by the Chilean Edmundo Marichal, and fitted with an Anzani Y 35hp engine. Marichal had produced some modified Bleriots before constructing the “Estudiantil” in the spring of 1913. It was used by the school of military aviation and had the distinction of being involved in the first aerial collision in Argentina in late November 1913, in which it was destroyed.
The EM-10 Bielik (English: white-tailed eagle) is a low cost Polish military training aircraft prototype, designed by Edward Margański and built by Margański & Mysłowski Zakłady Lotnicze, first flown on 4 June 2003.
The single engine aircraft has a composite (mostly carbon fibre) fuselage with a light alloy aft section and the pressurized cockpit is fitted with ejection seats.
Only one was built, now residing in the Polish Aviation Museum.
EM-10 prototype
Powerplant: 1 × General Electric CJ610-6 turbojet, 13.5 kN (3,000 lbf) thrust
Wingspan: 6.60 m (21 ft 8 in)
Wing area: 11.90 sq.m (128.1 sq ft)
Length: 9.00 m (29 ft 6 in)
Height: 2.50 m (8 ft 2 in)
Aspect ratio: 3.7
Empty weight: 1,700 kg (3,748 lb)
Max takeoff weight: 2,500 kg (5,512 lb)
Fuel capacity: 850 kg (1,870 lb)
Maximum speed: 1,100 km/h (680 mph, 590 kn)
Maximum speed: Mach 0.9
Stall speed: 165 km/h (103 mph, 89 kn)
Ferry range: 2,500 km (1,600 mi, 1,300 nmi) with auxiliary tanks
Rate of climb: 45 m/s (8,900 ft/min)
Wing loading: 210.1 kg/m2 (43.0 lb/sq ft)
Crew: 2
The D. M. K. Marendaz designed four-seat Marendaz III was quite an advanced concept for 1937, but never went into production. Two were built by International Aircraft & Engineering Ltd. at Maidenhead 1937/1938. The first, uncompleted, prototype was destroyed in a factory fire while the second, G-AFGG, although exhibited at the 1938 RAeS garden party, was never completed. The engine was a DH Gipsy VI of 200hp.
Mk.III
Engine: Gipsy Six
Wingspan: 31 ft
Length: 31 ft
Seats: 4
Mk.IV
Engine: Gipsy Major
Wingspan: 31 ft
Length: 31 ft
Seats: 3
Marendaz company, at Barton-in-the-Clay, Bedfordshire, built prototype Marendaz Trainer two-seat monoplane which first flew December 1939 as G-AFZX c/n A.B.T.1.
The only one built, it was given to the Halton Squadron of the Air Training Corps.
Engine: Blackburn Cirrus Minor I, 90 hp
Span: 34 ft 0 in
Length: 22 ft 4 in
Empty weight: 960 lb
AUW: 1500 lb
Max speed: 124 mph
Cruise: 95 mph
The Marcotte Rich Mixture II registered N91111 was an original single-seat biplane design by 35 year-old Ken Marcotte, an airframe and engine mechanic from Bedford Park, Ill, USA.
It had wood wings. Steel tube fuselage and tail, with Razorback cover. Fibreglass cowl and wheel fairings were fitted.
Engine: Continental C85-12
Wingspan: 19 ft / 5.79 m
Length: 17 ft / 5.18 m
Empty weight: 625 lb / 283.5 kg
MAUW: 1000 lb / 453.6 kg
Cruise: 115 mph / 185 kph
Landing speed: 50 mph / 80 kph
ROC: 1500 fpm / 7.62 m/sec
Range: 300 mi / 483 km
A two seat side by side, open frame gyrocopter.
Engine: 150-160 hp Lycoming.
Rotor blades: Rotordyne.
Min speed: 18 mph.
Cruise: 85 mph.
Top speed: 110 mph.
Empty wt: 625 lbs.
Useful load: 525 lbs.
Gross wt: 1150 lbs.
Width: 6’8”.
Length: 11’2”.
The 1909 Marchetti “Chimera” biplane was designed and built by Marchetti in Italy.
In 1911 the French army wanted to have an aircraft easily transportable and quickly dismountable from one location to another by road or railway. It was also required that the aircraft could be reassembled quickly. Baron Edmond de Marçay and Emile Moonen simplified the problem by imagining a device with wings folding along the fuselage, which was triangular and completely covered. The pilot could fold the wings without help and afterwards, according to the inventors, drive the machine on the road like a car, using the steerable rear wheels. The machine was first presented at the 1911 exhibition.
