Main Menu

Hermanspann Chinook



Chinook S

The Chinook S, designed by Fred Hermanspann and Art Penz, first flew in 1996, as an improved version of the original Chinook of 1993. Approach control is by full deflection trailing edge flaps. Both the flaps and main wheel are hydraulically actuated. The sailplane has been used to study the effect of rain on airfoils, and dynamics at the stall.

Wing span: 17.37m / 57ft
Wing area: 13.29sq.m / 143sq.ft
Empty Weight: 286kg / 630lb
Payload: 190kg / 420lb
Gross Weight: 476kg / 1050lb
Wing Load: 35.82kg/sq.m / 7.34lb/sq.ft
Water Ballast: 0
L/DMax: 40 98 kph / 53 kt / 61 mph
MinSink: 0.73 m/s / 2.17 fps / 1.42 kt
Aspect ratio: 22.7
Airfoil: Wortmann FX67-K-170/17
Structure: aluminum, GFRP front fuselage
Seats: 2
No. Built: 1


Copyright © 2020 all-aero. All Rights Reserved.
Joomla! is Free Software released under the GNU General Public License.