About: Avia BH-7   Sponge Permalink

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

The Avia BH-7 was a prototype fighter aircraft built in Czechoslovakia in 1923. It was a parasol-wing monoplane developed in tandem with and as an alternative to the BH-6, which shared its fuselage and tail design. Like the BH-6, the BH-7 was involved in a number of serious crashes during its test programme, which led to its abandonment as a fighter. Undaunted, however, Avia used the design as the basis for a racing aircraft, shortening the wingspan by 1.4 m (4 ft 7 in) and fairing it directly into the top of the fuselage and dispensing with the cabane struts. This revised version was designated BH-7B and the fighter (retrospectively) as the BH-7A. When the design proved no more successful as a racer it was finally put to rest.

AttributesValues
rdf:type
rdfs:label
  • Avia BH-7
rdfs:comment
  • The Avia BH-7 was a prototype fighter aircraft built in Czechoslovakia in 1923. It was a parasol-wing monoplane developed in tandem with and as an alternative to the BH-6, which shared its fuselage and tail design. Like the BH-6, the BH-7 was involved in a number of serious crashes during its test programme, which led to its abandonment as a fighter. Undaunted, however, Avia used the design as the basis for a racing aircraft, shortening the wingspan by 1.4 m (4 ft 7 in) and fairing it directly into the top of the fuselage and dispensing with the cabane struts. This revised version was designated BH-7B and the fighter (retrospectively) as the BH-7A. When the design proved no more successful as a racer it was finally put to rest.
sameAs
empty weight kg
  • 855(xsd:integer)
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
range km
  • 480(xsd:integer)
ceiling ft
  • 26200(xsd:integer)
climb rate ftmin
  • 1312(xsd:integer)
met or eng?
  • met
range miles
  • 300(xsd:integer)
eng1 type
  • Skoda licence-built Hispano-Suiza 8Fb Vee-8
gross weight kg
  • 1150(xsd:integer)
length in
  • 5(xsd:integer)
Type
  • Fighter
eng1 kW
  • 310(xsd:integer)
wing area sqft
  • 195(xsd:integer)
height m
  • 2(xsd:double)
Height in
  • 3(xsd:integer)
span m
  • 10(xsd:double)
climb rate ms
  • 6(xsd:double)
Manufacturer
  • Avia
max speed kmh
  • 240(xsd:integer)
empty weight lb
  • 1885(xsd:integer)
ceiling m
  • 8000(xsd:integer)
length m
  • 6(xsd:double)
max speed mph
  • 149(xsd:integer)
length ft
  • 22(xsd:integer)
Height ft
  • 9(xsd:integer)
First Flight
  • 1923(xsd:integer)
span ft
  • 34(xsd:integer)
gross weight lb
  • 2537(xsd:integer)
span in
  • 1(xsd:integer)
wing area sqm
  • 18(xsd:double)
Crew
  • one pilot
Armament
  • 2(xsd:integer)
Number Built
  • 2(xsd:integer)
eng1 hp
  • 231(xsd:integer)
Designer
  • Pavel Beneš and Miroslav Hajn
eng1 number
  • 1(xsd:integer)
abstract
  • The Avia BH-7 was a prototype fighter aircraft built in Czechoslovakia in 1923. It was a parasol-wing monoplane developed in tandem with and as an alternative to the BH-6, which shared its fuselage and tail design. Like the BH-6, the BH-7 was involved in a number of serious crashes during its test programme, which led to its abandonment as a fighter. Undaunted, however, Avia used the design as the basis for a racing aircraft, shortening the wingspan by 1.4 m (4 ft 7 in) and fairing it directly into the top of the fuselage and dispensing with the cabane struts. This revised version was designated BH-7B and the fighter (retrospectively) as the BH-7A. When the design proved no more successful as a racer it was finally put to rest.
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