The 1911 Marinescu 3-seat bomber monoplane was designed and built by Corneliu Martinescu in Romania.
Span: 30’2″
Length: 27’5″
Marinescu Bomber monoplane
Engines – Power
Marinens M.F.12
1939
Engine: 1 x 225hp Jacobs L-4B
Wingspan: 13.60 m / 45 ft 7 in
Length: 9.73 m / 32 ft 11 in
Height: 2.60 m / 9 ft 6 in
Max take-off weight: 2852 kg / 6288 lb
Empty weight: 1847 kg / 4072 lb
Max. speed: 230 km/h / 143 mph
Cruise speed: 195 km/h / 121 mph
Crew: 2
Marinens M.F.11
1931
Engine: 1 x 525hp Armstrong Siddeley Panther IIA
Wingspan: 10.55/15.41 m / 35 ft 7 in / 51 ft 7 in
Length: 11.63 m / 38 ft 2 in
Height: 4.45 m / 15 ft 7 in
Wing area: 53.50 sq.m / 575.87 sq ft
Max take-off weight: 2852 kg / 6288 lb
Empty weight: 1847 kg / 4072 lb
Max. speed: 235 km/h / 146 mph
Cruise speed: 170 km/h / 106 mph
Ceiling: 5000 m / 16400 ft
Range: 800 km / 497 miles
Range w/max.fuel: 1200 km / 746 miles
Armament: 3 x 7.92mm, 300kg of bombs
Crew: 3
Marinens M.F.10
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
Marinens M.F.8
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
Marinavia Farina QR.14 Levriero
Marinavia Farina Srl designed and built the prototype QR.14 Levriero four seat touring aircraft, powered by two de Havilland Gipsy Major 10 engines, first flown 1947, in which year it won Coppa dell’Aria at Milan.
Marichal Estudiantil
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.
Margański & Mysłowski EM-10 Bielik
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
Marendaz Mk.III / Mk.IV
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 Trainer
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
