About: Armstrong Whitworth AW.681

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About: Armstrong Whitworth AW.681 Sponge Permalink

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

The Armstrong Whitworth AW.681, also known as the Whitworth Gloster 681 or Hawker Siddeley HS.681, was a projected British long-range STOL military transport aircraft design by Armstrong Whitworth Aircraft and was to be capable of development to VTOL performance. The AW.681 was designed to meet the NATO specification BMR-4.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	Armstrong Whitworth AW.681
rdfs:comment	The Armstrong Whitworth AW.681, also known as the Whitworth Gloster 681 or Hawker Siddeley HS.681, was a projected British long-range STOL military transport aircraft design by Armstrong Whitworth Aircraft and was to be capable of development to VTOL performance. The AW.681 was designed to meet the NATO specification BMR-4.
sameAs	dbr:Armstrong_Whitworth_AW.681
dcterms:subject	dbkwik:resource/CxlkLvL1w_ROLWNo-ZxR0A== dbkwik:resource/dE4SR41P3VcvZpsifT_bpQ== dbkwik:resource/X-iLEAJ7jXFr_RQwRXyRdw== dbkwik:resource/tNDrA85DvL_7GZoFXjpONA== dbkwik:resource/fMV2sIx8SfH505BDncFuAg== dbkwik:resource/7ogZWGJnmaNiKHT7PlSAsw==
dbkwik:military/pr...iPageUsesTemplate	dbkwik:resource/AaGpNMKXeCEx6k1ovZIRVg== dbkwik:resource/ODD2urn6xOTu5tfNx3dKHA== dbkwik:resource/pTEKXoXwy_QJD-cbbKl3EQ== dbkwik:resource/CtbfVERA8rrkkb3qmAFx5A== dbkwik:resource/8c65HClsHBgkxfJdWXaRHw== dbkwik:resource/cbsrEQx1xy51eXd2rIQtLg== dbkwik:resource/sgy-37hYEWSi0ff69o00Qg== dbkwik:resource/7_dwHHF8FUA3XhGjI4-8Fw==
max takeoff weight alt	82360.0
max speed more	457200.0
length alt	31(xsd:double)
span main	134.0
Status	Project cancelled February 1965
thrust alt	61.3 kN
height alt	11.53 m
Type	Projected VTOL Military transport
range alt	7725.0
length main	3175.0
area main	2250.0
height main	1153.16
span alt	40(xsd:double)
payload alt	15900.0
range main	4801.0
Manufacturer	Hawker Siddeley
max speed main	Mach 0.71
ceiling main	25000.0
type of jet	turbofans with thrust deflection
area alt	209.0
engine (jet)	dbkwik:resource/2vgb9pim1AbdTb-Hrcdqsg==
jet or prop?	jet
thrust main	13790.0
number of jets	4(xsd:integer)
plane or copter?	plane
ceiling alt	7,620 m
max takeoff weight main	181200.0
payload main	35000.0
ref	Armstrong Whitworth Aircraft since 1913
abstract	The Armstrong Whitworth AW.681, also known as the Whitworth Gloster 681 or Hawker Siddeley HS.681, was a projected British long-range STOL military transport aircraft design by Armstrong Whitworth Aircraft and was to be capable of development to VTOL performance. The AW.681 was designed to meet the NATO specification BMR-4.

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