About: Brantly B-2

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About: Brantly B-2 Sponge Permalink

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

The Brantly B-2 is an American two-seat light helicopter produced by the Brantly Helicopter Corporation.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	Brantly B-2
rdfs:comment	The Brantly B-2 is an American two-seat light helicopter produced by the Brantly Helicopter Corporation. The B-2 was designed in the early 1950s by Newby Brantly as a simple two-seat light helicopter, simpler than his earlier B-1. The first example flew on 21 February 1953, and the aircraft received certification in 1959, with production beginning shortly after. A five-seat version with a more powerful engine was developed in the early 1960s and called the 305. Production initially ended in the early 1970s, but was resumed in 1976 after Brantly was acquired by Michael Hynes and renamed Brantly-Hynes. B-2s continue to be built today, with over 400 examples already in service.
sameAs	dbr:Brantly_B-2
dcterms:subject	Helicopter Civilian aircraft dbkwik:resource/m6fVF57RpnoQLv0sb2yYXg== American Aircraft dbkwik:resource/g75r3Q-JiKaPn6xhA3TOdw== dbkwik:resource/jyrsqnIZzR9knGh_BFIXDA== dbkwik:resource/bxkP9KST7Pzuxm5tpHLrXA==
dbkwik:military/pr...iPageUsesTemplate	dbkwik:resource/AaGpNMKXeCEx6k1ovZIRVg== dbkwik:resource/pTEKXoXwy_QJD-cbbKl3EQ== dbkwik:resource/8c65HClsHBgkxfJdWXaRHw== dbkwik:resource/cbsrEQx1xy51eXd2rIQtLg== dbkwik:resource/A6jzNLH0bAeBL_XaRLe6Kg== dbkwik:resource/7_dwHHF8FUA3XhGjI4-8Fw==
max takeoff weight alt	757.0
max speed more	at sea level
climb rate main	1900.0
number of props	1(xsd:integer)
length alt	6.63 m
span main	723.9
Status	In production
cruise speed main	90.0
cruise speed alt	78(xsd:integer)
height alt	2.06 m
Introduced	1958(xsd:integer)
Type	Light Helicopter
type of prop	air-cooled flat-four piston
range alt	217(xsd:integer)
length main	662.94
power alt	134(xsd:integer)
Unit Cost	$19,950 in 1962
area main	442.0
power main	180.0
height main	205.74
span alt	7.24 m
range main	250.0
Manufacturer	dbkwik:resource/_akdfdsnFbe4gn7xfjEVJg==
max speed main	100.0
engine (prop)	dbkwik:resource/OV_Uh6TCaPaNdFc9Cki9Cg==
climb rate alt	9.7
ceiling main	10800.0
empty weight main	1020.0
area alt	41.06
First Flight	1953-02-21(xsd:date)
max speed alt	87(xsd:integer)
jet or prop?	prop
empty weight alt	463.0
plane or copter?	copter
ceiling alt	3290 m
max takeoff weight main	1670.0
cruise speed more
Designer	dbkwik:resource/Zf3D9983hmWMCz8fA5h3_g==
ref	Jane's All The World's Aircraft 1976-77
abstract	The Brantly B-2 is an American two-seat light helicopter produced by the Brantly Helicopter Corporation. The B-2 was designed in the early 1950s by Newby Brantly as a simple two-seat light helicopter, simpler than his earlier B-1. The first example flew on 21 February 1953, and the aircraft received certification in 1959, with production beginning shortly after. A five-seat version with a more powerful engine was developed in the early 1960s and called the 305. Production initially ended in the early 1970s, but was resumed in 1976 after Brantly was acquired by Michael Hynes and renamed Brantly-Hynes. B-2s continue to be built today, with over 400 examples already in service. The United States Army evaluated the B-2 in 1958 as the YHO-3, but found it to be unsuitable for their needs and placed no orders.

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