About: Gabardini G.9   Sponge Permalink

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

Gabardini designed the G.9 in parallel with its work on its first fighter design, the Gabardini G.8, which had a similar wing cellule. The G.9 was a metal, fabric-covered, single-bay biplane which differed from the unequal-span G.8 in having a shorter-span upper wing and less cabane bracing. It was powered by the 164-kilowatt (220-horsepower) SPA 6a engine—a more powerful engine than that of any G.8 variant—driving a two-bladed propeller. The Regia Aeronautica (Italian Royal Air Force) did not place a production order for the G.9

AttributesValues
rdf:type
rdfs:label
  • Gabardini G.9
rdfs:comment
  • Gabardini designed the G.9 in parallel with its work on its first fighter design, the Gabardini G.8, which had a similar wing cellule. The G.9 was a metal, fabric-covered, single-bay biplane which differed from the unequal-span G.8 in having a shorter-span upper wing and less cabane bracing. It was powered by the 164-kilowatt (220-horsepower) SPA 6a engine—a more powerful engine than that of any G.8 variant—driving a two-bladed propeller. The Regia Aeronautica (Italian Royal Air Force) did not place a production order for the G.9
sameAs
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
eng1 note
  • :::G.9bis - 1 x Hispano-Suiza HS42 V-8 water-cooled piston engine
time to altitude
  • 900.0
eng1 type
  • 6(xsd:integer)
Type
  • Fighter and trainer
max speed note
  • :::G.9bis -
eng1 kW
  • 164(xsd:integer)
span m
  • 7(xsd:integer)
climb rate ms
  • 5(xsd:double)
Manufacturer
max speed kmh
  • 235(xsd:integer)
length m
  • 6(xsd:integer)
National Origin
  • Italy
First Flight
  • 1923(xsd:integer)
wing area sqm
  • 18(xsd:integer)
prime units?
  • met
Crew
  • 1(xsd:integer)
eng1 name
Designer
eng1 number
  • 1(xsd:integer)
abstract
  • Gabardini designed the G.9 in parallel with its work on its first fighter design, the Gabardini G.8, which had a similar wing cellule. The G.9 was a metal, fabric-covered, single-bay biplane which differed from the unequal-span G.8 in having a shorter-span upper wing and less cabane bracing. It was powered by the 164-kilowatt (220-horsepower) SPA 6a engine—a more powerful engine than that of any G.8 variant—driving a two-bladed propeller. The Regia Aeronautica (Italian Royal Air Force) did not place a production order for the G.9
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