About: Curtiss P-60

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About: Curtiss P-60 Sponge Permalink

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

The Curtiss P-60 was a 1940s United States single-engine single-place, low-wing monoplane fighter aircraft developed by the Curtiss-Wright company as a successor to their P-40. It went through a lengthy series of prototype versions, eventually evolving into a design that bore little resemblance to the P-40. None of these versions reached production.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	Curtiss P-60
rdfs:comment	The Curtiss P-60 was a 1940s United States single-engine single-place, low-wing monoplane fighter aircraft developed by the Curtiss-Wright company as a successor to their P-40. It went through a lengthy series of prototype versions, eventually evolving into a design that bore little resemblance to the P-40. None of these versions reached production.
sameAs	dbr:Curtiss_P-60
dcterms:subject	dbkwik:resource/m76mbrD_xDYDGSevT3g-RQ== dbkwik:resource/CPFubkChK8CCDYNywaDjow== dbkwik:resource/n4zNcgGt7LLRn6wZC2LapQ== dbkwik:resource/pjtdewig2qBxp2WkiBIfvw== dbkwik:resource/Pl38NLrWVrtpalEM90J-Hw==
dbkwik:military/pr...iPageUsesTemplate	dbkwik:resource/AaGpNMKXeCEx6k1ovZIRVg== dbkwik:resource/pTEKXoXwy_QJD-cbbKl3EQ== dbkwik:resource/j8B-K-oAVfK2X6QH23Gdjg== dbkwik:resource/CtbfVERA8rrkkb3qmAFx5A== dbkwik:resource/8c65HClsHBgkxfJdWXaRHw== dbkwik:resource/cbsrEQx1xy51eXd2rIQtLg== dbkwik:resource/sgy-37hYEWSi0ff69o00Qg== dbkwik:resource/7_dwHHF8FUA3XhGjI4-8Fw==
loaded weight main	10785.0
Guns	4(xsd:integer)
climb rate main	3890.0
number of props	1(xsd:integer)
length alt	10.34 m
span main	41.33
power/mass alt	300(xsd:integer)
Produced	1942(xsd:integer)
Status	Cancelled
height alt	3.76 m
primary user	United States Army Air Forces
Type	Fighter aircraft
type of prop	radial engine
loading main	39(xsd:double)
Program Cost	$8.88 million USD
length main	33.92
power alt	1492.0
area main	275.0
power main	2000.0
height main	12.33
span alt	12.60 m
Manufacturer	Curtiss-Wright
max speed main	414.0
engine (prop)	Pratt & Whitney R-2800-53
power/mass main	0(xsd:double)
climb rate alt	19.8
ceiling main	37900.0
empty weight main	8698.0
loaded weight alt	4892.0
Developed From	Curtiss XP-46 Curtiss XP-53
area alt	25.6
First Flight	1941-09-18(xsd:date)
max speed alt	360(xsd:integer)
jet or prop?	prop
loading alt	191(xsd:integer)
empty weight alt	3945.0
plane or copter?	plane
ceiling alt	11,600 m
Retired	1944-12-22(xsd:date)
Crew	1(xsd:integer)
Number Built	5(xsd:integer)
abstract	The Curtiss P-60 was a 1940s United States single-engine single-place, low-wing monoplane fighter aircraft developed by the Curtiss-Wright company as a successor to their P-40. It went through a lengthy series of prototype versions, eventually evolving into a design that bore little resemblance to the P-40. None of these versions reached production.
is Developed Into of	Curtiss XP-46

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