Back Kaman K-17
1958

Kaman K-17

Experimental two-seater built in 1958 powered by a "cold-jet" rotor system: the 400 hp Blackburn Turbomeca Turmo 600 turbine drove a compressor which fed compressed air to blade-tip nozzles.

G.Apostolo "The Illustrated Encyclopedia of Helicopters", 1984

*     *     *

Technical data for K-17

Engine: 1 x Blackburn/Turbomeca "Turmo" turboshaft, rated at 300kW, main rotor diameter: 11.28m, length: 7.01m, height: 3.35m, empty weight: 431kg, take-off weight: 907kg, max speed: 129km/h, ceiling: 1525m, range: 250km

Comments 
Leland Crowl, e-mail, 14.08.2015

What nozzle pressure did it have and what was the rotor rpm?

shoes, e-mail, 14.06.2011

i am learn from here!

peter, e-mail, 03.02.2009

put more facts

Do you have any comments concerning this aircraft ?

Name   E-mail


All the World's Rotorcraft


Virtual Aircraft Museum


Back AVIATION TOP 100 - www.avitop.com Avitop.com