About: Fokker DC.I   Sponge Permalink

An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

{| |} The Fokker DC.I was an aircraft produced in the Netherlands in the early 1920s to fulfill a role of combined fighter and reconnaissance aircraft. The company designation chosen by Fokker, "DC" reflected this, with "D" being the Idflieg designation for a fighter during World War I, and "C" being an armed reconnaissance aircraft. The DC.I was a conventional single-bay biplane with staggered, unequal-span wings braced by N-struts and was derived from the Fokker C.IV design. The pilot and observer sat in tandem, open cockpits, and the undercarriage was of fixed, tailskid configuration, with the main units linked by a cross-axle. The wings were of wooden construction, and the fuselage was of welded steel tube covered in fabric.

AttributesValues
rdf:type
rdfs:label
  • Fokker DC.I
rdfs:comment
  • {| |} The Fokker DC.I was an aircraft produced in the Netherlands in the early 1920s to fulfill a role of combined fighter and reconnaissance aircraft. The company designation chosen by Fokker, "DC" reflected this, with "D" being the Idflieg designation for a fighter during World War I, and "C" being an armed reconnaissance aircraft. The DC.I was a conventional single-bay biplane with staggered, unequal-span wings braced by N-struts and was derived from the Fokker C.IV design. The pilot and observer sat in tandem, open cockpits, and the undercarriage was of fixed, tailskid configuration, with the main units linked by a cross-axle. The wings were of wooden construction, and the fuselage was of welded steel tube covered in fabric.
sameAs
empty weight kg
  • 1400(xsd:integer)
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
ceiling ft
  • 26250(xsd:integer)
met or eng?
  • met
eng1 type
endurance h
  • 3(xsd:integer)
gross weight kg
  • 1830(xsd:integer)
length in
  • 1(xsd:integer)
primary user
Type
  • Fighter and reconnaissance aircraft
eng1 kW
  • 340(xsd:integer)
height m
  • 3(xsd:double)
Height in
  • 2(xsd:integer)
span m
  • 11(xsd:double)
Manufacturer
max speed kmh
  • 245(xsd:integer)
empty weight lb
  • 3090(xsd:integer)
ceiling m
  • 8000(xsd:integer)
length m
  • 8(xsd:double)
max speed mph
  • 152(xsd:integer)
length ft
  • 29(xsd:integer)
Height ft
  • 11(xsd:integer)
span ft
  • 38(xsd:integer)
gross weight lb
  • 4030(xsd:integer)
span in
  • 7(xsd:integer)
Crew
  • Two - pilot and observer
Armament
  • 1(xsd:integer)
  • 2(xsd:integer)
Number Built
  • 10(xsd:integer)
eng1 hp
  • 450(xsd:integer)
Designer
eng1 number
  • 1(xsd:integer)
abstract
  • {| |} The Fokker DC.I was an aircraft produced in the Netherlands in the early 1920s to fulfill a role of combined fighter and reconnaissance aircraft. The company designation chosen by Fokker, "DC" reflected this, with "D" being the Idflieg designation for a fighter during World War I, and "C" being an armed reconnaissance aircraft. The DC.I was a conventional single-bay biplane with staggered, unequal-span wings braced by N-struts and was derived from the Fokker C.IV design. The pilot and observer sat in tandem, open cockpits, and the undercarriage was of fixed, tailskid configuration, with the main units linked by a cross-axle. The wings were of wooden construction, and the fuselage was of welded steel tube covered in fabric. Ten DC.Is were ordered by the Dutch East Indies Army Air Service, which flew them from 1925 to 1934.
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