VS-300 is equipped with 3-bladed main rotor of 141ft radius and has welded tubular steel fuselage; 90-hp Franklin air cooled engine replaces previous 75-hp engine; practical results of 1941 are demonstrated by brief resume of flights made. (See also J Aeronautical Sciences v 9 n 8 June 1942 p 309-11; Flight v 42 n 1758 Sept 3 1942 p 261-3; Am Academy Arts and Sciences -- Proc v 75 n 1 Oct 1942 p 21-2)
Technical development of VS-300 helicopter during 1941
Automotive Aviation Industries
Automotive and Aviation Industries ; 86 , n 7
1942
Article (Journal)
English
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