The Albatros L 75 Ass (German: "Ace") was a German trainerbiplane of the 1920s. Of conventional configuration, it seated the pilot and instructor in separate, open cockpits. The wings were single-bay, equal-span, and had a slight stagger. Production continued after Albatros was absorbed by Focke-Wulf.
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^Grey, C.G., ed. (1928). Jane's all the World's Aircraft 1928. London: Sampson Low, Marston & company, ltd. p. 128c.
^"Albatros L 75". histaviation.com. Retrieved 9 February 2018.
Further readingedit
Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 56.
December 15, 2023
albatros, german, german, trainer, biplane, 1920s, conventional, configuration, seated, pilot, instructor, separate, open, cockpits, wings, were, single, equal, span, slight, stagger, production, continued, after, albatros, absorbed, focke, wulf, assrole, trai. The Albatros L 75 Ass German Ace was a German trainer biplane of the 1920s Of conventional configuration it seated the pilot and instructor in separate open cockpits The wings were single bay equal span and had a slight stagger Production continued after Albatros was absorbed by Focke Wulf L 75 AssRole TrainerManufacturer Albatros FlugzeugwerkeDesigner Walter BlumeFirst flight 1928Number built 43Variants editL 75 prototype with BMW IVa engine L 75a production version with BMW Va engine L 75b with Junkers L5 engine L 75c BMW Va engine L 75d BMW Va engine L 75E BMW Va engine L 75F Junkers L5G engine L 75DSA BMW Va engine L 75DSB Junkers L5 engineOperators editDVSSpecifications L 75a edit nbsp Albatros L 75 drawing from Le Document aeronautique November 1928Data from Jane s all the World s Aircraft 1928 1 German Aircraft between 1919 1945 2 General characteristicsCrew 2 Length 10 m 32 ft 10 in Wingspan 12 5 m 41 ft 0 in Height 3 25 m 10 ft 8 in Wing area 37 m2 400 sq ft Empty weight 1 150 kg 2 535 lb Gross weight 1 835 kg 4 045 lb Fuel capacity 480 L 130 US gal 110 imp gal main 93 L 25 US gal 20 imp gal in reserve gravity feed tank Powerplant 1 BMW Va six cylinder in line water cooled piston engine 270 kW 360 hp for take off 240 kW 320 hp continuous Propellers 2 bladed fixed pitch propellerPerformance Maximum speed 217 km h 135 mph 117 kn Cruise speed 170 km h 110 mph 92 kn Landing speed 90 km h 56 mph 49 kn Range 1 600 km 990 mi 860 nmi Service ceiling 5 500 m 18 000 ft Time to altitude 1 000 m 3 300 ft in 7 minutes Wing loading 59 8 kg m2 12 2 lb sq ft Power mass 0 1141 kW kg 0 0694 hp lb References edit nbsp Wikimedia Commons has media related to Albatros L 75 Grey C G ed 1928 Jane s all the World s Aircraft 1928 London Sampson Low Marston amp company ltd p 128c Albatros L 75 histaviation com Retrieved 9 February 2018 Further reading editTaylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions p 56 Retrieved from https en wikipedia org w index php title Albatros L 75 amp oldid 1125780758, wikipedia, wiki, book, books, library,
