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Ikarus AD Meteor
 
Ikarus-Meteor
 
The all-metal Meteor was designed in 1954 by Boris Cijan, Stanko Obad and Miho Mazovec. The Meteor high performance single-seater with its laminar flow wing, camber-changing flaps and very slim fuselage to give minimum cross sectional area set a pattern for the high performance types of today when it first flew from Belgrade on 4 May 1956. It soon made its mark in competition flying, taking fourth or fifth place in the Open Class in the World Championships of 1956, 1958 and 1960 and for a time it held the world speed records for the 100 and 300km triangular closed circuits.
 
The ailerons are divided into inboard and outboard sections, of which the inner sections can be drooped in conjunction with the flaps for landing, and modified DFS-type air brakes are fitted in the wing upper surfaces. The semi-monocoque all-metal fuselage is built in two sections for ease of repair, the rear section being straight tapered with stringers and a stressed skin. The landing gear consists of a bow-shaped front skid that extends some way out from under the forward fuselage, and a retractable monowheel with brake. The pilot is seated under a detachable one-piece canopy.
 
Meteor 60
Span: 65ft 7.5in / 20.0 m
Length: 26ft 5in / 8.05 m
Wing area: 172.2 sqft / 16.0 sq.m
Aspect ratio: 25.0
Wing section: NACA 633 616 5
Empty weight: 829 lb / 376 kg
Max weight: 1,113 lb / 505 kg
Water ballast: None
Max wing loading: 31.5 kg/sq.m / 6.45 lb/sq ft
Max speed: 135 kt / 250 km/h / 155 mph (in smooth air)
Max rough air speed: 67.5 kt / 125 km/h
Stalling speed: 36 kt / 67 km/h
Min sinking speed: 1.77ft/sec / 0.54 m/sec
Best glide ratio: 42:1 at 56mph / 48.5 kt / 90 km/h
 

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