The Arado Ar 199 was a floatplane aircraft, built by Arado Flugzeugwerke. It was a low-wing monoplane, designed in 1938 to be launched from a catapult and operated over water. The enclosed cockpit had two side-by-side seats for instructor and student, and a third, rear seat, for a trainee-navigator or radio operator.
^Tilford Jr., Earl (1977). . Air University Review (January - February 1977). United States Air Force. Archived from the original on 2017-01-13.
^Green, William (2010). Aircraft of the Third Reich. Vol. 1 (1st ed.). London: Aerospace Publishing Limited. pp. 56–57. ISBN978-1-900732-06-2.
Bibliography
Smith, J R; Kay, Antony L. (1972). German Aircraft of the Second World War. London: Putnam. ISBN978-0-85177-836-5.
January 01, 1970
arado, floatplane, aircraft, built, arado, flugzeugwerke, wing, monoplane, designed, 1938, launched, from, catapult, operated, over, water, enclosed, cockpit, side, side, seats, instructor, student, third, rear, seat, trainee, navigator, radio, operator, model. The Arado Ar 199 was a floatplane aircraft built by Arado Flugzeugwerke It was a low wing monoplane designed in 1938 to be launched from a catapult and operated over water The enclosed cockpit had two side by side seats for instructor and student and a third rear seat for a trainee navigator or radio operator Ar 199 Model of an Ar 199 Role Trainer National origin Germany Manufacturer Arado Flugzeugwerke First flight 1939 1 Primary user Luftwaffe Number built 31 2 3 Two of the 5 prototypes D IFRB and D ISBC did serve as trainers 1 and were used for air sea rescue operations from Northern Norway 4 Specifications Ar 199 editData from Aircraft of the Third Reich Vol 1 5 General characteristicsCrew three Length 10 57 m 34 ft 8 in Wingspan 12 7 m 41 ft 8 in Height 4 36 m 14 ft 4 in Wing area 30 4 m2 327 sq ft Empty weight 1 675 kg 3 693 lb Max takeoff weight 2 075 kg 4 575 lb Powerplant 1 Argus As 410C inverted V 12 air cooled piston engine 340 kW 450 hp Propellers 2 bladed variable pitch propeller Performance Maximum speed 260 km h 160 mph 140 kn at 3 000 m 9 800 ft Cruise speed 212 km h 132 mph 114 kn Range 740 km 460 mi 400 nmi Service ceiling 6 500 m 21 300 ft Rate of climb 4 5 m s 890 ft min Time to altitude 3 000 m 9 800 ft in 11 minutesReferences edit nbsp Wikimedia Commons has media related to Arado Ar 199 Notes a b Smith 1972 p 34 Jorg Armin Kranzhoff Arado Geschichte eines Flugzeugwerks Aviatic Verlag Oberhaching Germany 1995 ISBN 3 925505 27 X Jorg Armin Kranzhoff Arado 96 Varianten In Flugzeug Profile 43 UNITEC Medienvertrieb Stengelheim Germany Tilford Jr Earl 1977 SEENOTDIENST Early Development of Air Sea Rescue Air University Review January February 1977 United States Air Force Archived from the original on 2017 01 13 Green William 2010 Aircraft of the Third Reich Vol 1 1st ed London Aerospace Publishing Limited pp 56 57 ISBN 978 1 900732 06 2 Bibliography Smith J R Kay Antony L 1972 German Aircraft of the Second World War London Putnam ISBN 978 0 85177 836 5 Retrieved from https en wikipedia org w index php title Arado Ar 199 amp oldid 1192842695, wikipedia, wiki, book, books, library,
