About: IVL C.VI.25

Description
Metadata
Settings
- owl:sameAs
- Inference Rule:

About: IVL C.VI.25 Sponge Permalink

An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : dbkwik.org associated with source dataset(s)

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.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	IVL C.VI.25
rdfs:comment	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.
sameAs	dbr:IVL_C.VI.25
dcterms:subject	dbkwik:resource/HTMXQqehGg8Awsq7Fg5RqA== dbkwik:resource/m76mbrD_xDYDGSevT3g-RQ== dbkwik:resource/-6gdGXUPe5gRNEIHm1dFJQ== dbkwik:resource/dE4SR41P3VcvZpsifT_bpQ==
dbkwik:military/pr...iPageUsesTemplate	dbkwik:resource/AaGpNMKXeCEx6k1ovZIRVg== dbkwik:resource/nxqfX2A3Or3bCbgXY02qvg== dbkwik:resource/pTEKXoXwy_QJD-cbbKl3EQ== dbkwik:resource/8c65HClsHBgkxfJdWXaRHw== dbkwik:resource/cbsrEQx1xy51eXd2rIQtLg== dbkwik:resource/7_dwHHF8FUA3XhGjI4-8Fw==
max takeoff weight alt	1854.0
loaded weight main	kg
climb rate main	m/s
number of props	1(xsd:integer)
length alt	685.8000000000001
span main	9.5 m
power/mass alt	hp/lb
Status	--12-17
cruise speed main	km/h
cruise speed alt	knots, mph
height alt	ft in
primary user	Finnish Air Force
Type	Fighter aircraft
type of prop	radial engine
loading main	kg/m²
range alt	nm, mi
length main	6.9 m
useful load main	kg
power alt	160.0
area main	m²
power main	119.0
stall speed alt	knots, mph
height main	m
span alt	949.96
range main	km
Manufacturer	dbkwik:resource/yGweDEZ6_3UITW1EfLZh8A==
max speed main	210.0
engine (prop)	Siemens-Halske Sh.IIIA
power/mass main	W/kg
climb rate alt	ft/min
ceiling main	m
empty weight main	kg
stall speed main	km/h
loaded weight alt	lb
Developed From	IVL C.24
area alt	ft²
First Flight	1925-06-11(xsd:date)
max speed alt	113(xsd:integer)
jet or prop?	prop
never exceed speed alt	knots, mph
loading alt	lb/ft²
empty weight alt	lb
plane or copter?	plane
ceiling alt	ft
max takeoff weight main	843.0
never exceed speed main	km/h
Crew	1(xsd:integer)
Number Built	1(xsd:integer)
ref	Thulinista Hornettiin
useful load alt	kg
abstract	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.

OpenLink Virtuoso version 07.20.3217, on Linux (x86_64-pc-linux-gnu), Standard Edition
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2012 OpenLink Software