About: Avia BH-8

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

The Avia BH-8 was a prototype fighter aircraft built in Czechoslovakia in 1923. It was an unequal-span biplane developed on the basis of the ill-fated BH-6 design, in an attempt to address that type's problems. It shared the BH-6's unusual wing cellule design. When test-flown in late 1923, it did indeed display better flying characteristics than its predecessor, but was overtaken in development by another variation on the same design, the BH-17.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	Avia BH-8
rdfs:comment	The Avia BH-8 was a prototype fighter aircraft built in Czechoslovakia in 1923. It was an unequal-span biplane developed on the basis of the ill-fated BH-6 design, in an attempt to address that type's problems. It shared the BH-6's unusual wing cellule design. When test-flown in late 1923, it did indeed display better flying characteristics than its predecessor, but was overtaken in development by another variation on the same design, the BH-17.
sameAs	dbr:Avia_BH-8
empty weight kg	843(xsd:integer)
dcterms:subject	dbkwik:resource/FUwnXua-41_8iqKSDDJhpQ== dbkwik:resource/GwnN8Y-ExwLeIcbR5G9o9w== dbkwik:resource/dgGPtw1rSSE8PvrGDGr_xQ== dbkwik:resource/Nz-_L8VvN7csoPCds0-ZUQ==
dbkwik:military/pr...iPageUsesTemplate	dbkwik:resource/AaGpNMKXeCEx6k1ovZIRVg== dbkwik:resource/ODD2urn6xOTu5tfNx3dKHA== dbkwik:resource/8c65HClsHBgkxfJdWXaRHw== dbkwik:resource/5lvlPxSCz0xGKWOtWRKF6g== dbkwik:resource/7_dwHHF8FUA3XhGjI4-8Fw== dbkwik:resource/dLGY2ypVsQBpZ71XpuCB9g==
range km	450(xsd:integer)
ceiling ft	26200(xsd:integer)
climb rate ftmin	1115(xsd:integer)
met or eng?	met
range miles	280(xsd:integer)
eng1 type	Skoda licence-built Hispano-Suiza 8Fb Vee-8
gross weight kg	1143(xsd:integer)
length in	3(xsd:integer)
Type	Fighter
eng1 kW	310(xsd:integer)
wing area sqft	238(xsd:integer)
height m	2(xsd:double)
Height in	1(xsd:integer)
span m	9(xsd:double)
climb rate ms	5(xsd:double)
Manufacturer	Avia
max speed kmh	222(xsd:integer)
empty weight lb	1858(xsd:integer)
ceiling m	8000(xsd:integer)
length m	6(xsd:double)
max speed mph	138(xsd:integer)
length ft	21(xsd:integer)
Height ft	9(xsd:integer)
First Flight	1923(xsd:integer)
span ft	31(xsd:integer)
gross weight lb	2520(xsd:integer)
span in	1(xsd:integer)
wing area sqm	22(xsd:double)
Crew	one pilot
Armament	2(xsd:integer)
Number Built	1(xsd:integer)
eng1 hp	231(xsd:integer)
Designer	Pavel Beneš and Miroslav Hajn
eng1 number	1(xsd:integer)
abstract	The Avia BH-8 was a prototype fighter aircraft built in Czechoslovakia in 1923. It was an unequal-span biplane developed on the basis of the ill-fated BH-6 design, in an attempt to address that type's problems. It shared the BH-6's unusual wing cellule design. When test-flown in late 1923, it did indeed display better flying characteristics than its predecessor, but was overtaken in development by another variation on the same design, the BH-17.

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