The Hawk GafHawk ("General Aviation Freighter") was a small, turboprop-powered freighter aircraft developed in the United States in the 1980s but which only flew in prototype form. It was designed by as a means of transporting drilling equipment in and out of remote locations, and was designed to be simple, rugged, and have good STOL and rough-field performance. The resulting design was a boxy aircraft with a rectangular-section fuselage with a high-set tail and rear loading ramp. The high aspect-ratio wings were high-set and braced with struts. The landing gear was fixed and of tricycle configuration, with the main units having dual wheels.
Attributes | Values |
---|
rdf:type
| |
rdfs:label
| |
rdfs:comment
| - The Hawk GafHawk ("General Aviation Freighter") was a small, turboprop-powered freighter aircraft developed in the United States in the 1980s but which only flew in prototype form. It was designed by as a means of transporting drilling equipment in and out of remote locations, and was designed to be simple, rugged, and have good STOL and rough-field performance. The resulting design was a boxy aircraft with a rectangular-section fuselage with a high-set tail and rear loading ramp. The high aspect-ratio wings were high-set and braced with struts. The landing gear was fixed and of tricycle configuration, with the main units having dual wheels. (en)
|
dcterms:subject
| |
Wikipage page ID
| |
Wikipage revision ID
| |
Link from a Wikipage to another Wikipage
| |
Link from a Wikipage to an external page
| |
sameAs
| |
span ft
| |
span in
| |
stall speed mph
| |
stall speed note
| |
wing area sqft
| |
dbp:wikiPageUsesTemplate
| |
dbp:primeUnits%3F_
| |
first flight
| |
national origin
| |
crew
| |
height ft
| |
height in
| |
length ft
| |
manufacturer
| |
ref
| - Jane's All the World's Aircraft 1988–89 (en)
|
type
| |
has abstract
| - The Hawk GafHawk ("General Aviation Freighter") was a small, turboprop-powered freighter aircraft developed in the United States in the 1980s but which only flew in prototype form. It was designed by as a means of transporting drilling equipment in and out of remote locations, and was designed to be simple, rugged, and have good STOL and rough-field performance. The resulting design was a boxy aircraft with a rectangular-section fuselage with a high-set tail and rear loading ramp. The high aspect-ratio wings were high-set and braced with struts. The landing gear was fixed and of tricycle configuration, with the main units having dual wheels. Certification proved elusive, however, and Hawk eventually abandoned the project without building any other examples. (en)
|
aspect ratio
| |
ceiling ft
| |
climb rate ftmin
| |
climb rate note
| |
cruise speed mph
| |
cruise speed note
| |
empty weight lb
| |
eng1 hp
| |
eng1 name
| - Pratt & Whitney Canada PT6A-65B/R (en)
|
eng1 number
| |
gross weight lb
| |
length in
| |
more performance
| - *Take-off run to 50 ft :
*Landing run from 50 ft : (en)
|
number built
| |
range miles
| |
range note
| |
gold:hypernym
| |
prov:wasDerivedFrom
| |
page length (characters) of wiki page
| |
number built
| |
manufacturer
| |
foaf:isPrimaryTopicOf
| |
is Link from a Wikipage to another Wikipage
of | |
is Wikipage redirect
of | |
is foaf:primaryTopic
of | |