“IVL C.VI.25”的意思、由来-开放百科全书

词条

IVL C.VI.25

释义

Operators
Specifications (C.VI.25)
Sources
See also

name=C.VI.25

image=I.V.L. C.25 "Pikku hävittäjä" (35546406756).jpg

caption=

}}{{Infobox Aircraft Type

type=Fighter aircraft

manufacturer=IVL

designer=

first flight=June 11, 1925

introduced=

retired=

status=Destroyed on December 17, 1925

primary user=Finnish Air Force

more users=

produced=

number built=1

unit cost=

developed from=IVL C.24

variants with their own articles=
}}

IVL C.VI.25 was a Finnish fighter aircraft designed by IVL. It was a further development of the IVL C.24.

The aircraft made its maiden flight on June 11, 1925. The aircraft was wrecked after a forced landing, due to engine trouble, on December 17, 1925.

The aircraft was under-powered, like its predecessor, and it was not considered possible to further develop the aircraft.

Operators

{{FIN}}

Finnish Air Force

Specifications (C.VI.25)

{{aircraft specifications
|plane or copter?=plane
|jet or prop?=prop

|ref=Thulinista Hornettiin
|crew=1
|length main=6.9 m
|length alt= 22 ft 6 in
|span main=9.5 m
|span alt=31 ft 2 in
|max takeoff weight main=843 kg
|max takeoff weight alt=1,854 lb
|engine (prop)=Siemens-Halske Sh.IIIA
|type of prop=rotary engine
|number of props=1
|power main=119 kW
|power alt=160 hp
|max speed main=210 km/h
|max speed alt=113 knots, 130 mph
}}

Sources

Heinonen, Timo: Thulinista Hornetiin, Keski-Suomen ilmailumuseon julkaisuja 3, 1992. {{ISBN|951-95688-2-4}}.

Operators

Specifications (C.VI.25)

Sources

See also