NASA Ames Research Center conducted wind tunnel tests on the K-16B.
The sole Kaman K-16B is resting in the New England Air Museum, Hartford, Connecticut.
Engines: 2 x GE T-58-2A, 1024 hp
Wing span: 34 ft
Length: 38 ft 4 in
Height: 19 ft 3 in
Normal gross: 9295 lb
Design max speed SL: 211 kt
Deign max speed 15,000ft: 215 kt
Max ROC: 6000 fpm
Vertical climb: 400 fpm
Service ceiling: 36,000 ft
Hover ceiling: 2400 ft
Range w/1000lb fuel: 205 nm
Max range speed: 130 kt
TO to 50 ft 12,000 lb: 514 ft
Mean aerodynamic chord flap extended: 112.1 in
Prop Airfoil: NACA 16-500
Prop diameter: 14 ft 10 in
Prop blade chord: 18 in
Flapping hinge radius: 9.2%
Blade pitch range: 15-45 deg
Max wing tilt: 50 deg
Wing flap deflection: 60 deg
Rotor blade flap collective: 13 deg max
Rotor blade flap cyclic: +/- 25 deg
All Aero 