|
Entered service |
1985 |
|
Crew |
2 men |
|
Dimensions and weight |
|
Length |
14.2 m |
|
Main rotor diameter |
15.7
m |
|
Height |
4.12
m |
|
Weight (empty) |
3.3 t |
|
Weight (maximum take off) |
6.4 t |
|
Engines and performance |
|
Engines |
2 x PZL-10W turboshaft engines |
|
Engine power |
2 x 900 hp |
|
Maximum speed |
250 km/h |
|
Service ceiling |
5.1 km |
|
Range |
760 km |
|
Payload |
|
Maximum payload |
? |
|
Typical load |
12 passengers |
|
In 1979,
with nearly 20 years experience of building Mil-designed helicopters
behind it, Poland's PZL Swidnik flew the first prototype of a new
design designated W-3 and named Sokol (Flacon). There was a long
series of tethered tests and extensive design changes before the
second prototype flew in May 1982, and it was another three years
before production began. Since then, PZL has developed several
specialized variants for military and civil applications.
By 1996 PZL
had completed more than 80 production W-3s, including 12 for
Myanmar. Others were built for the Polish armed forces and
government agencies, and included naval, fire-fighting and search
and rescue (SAR) models.
Known as the
Anakonda, the W-3RM is a rescue variant with flotation bags, a
watertight cabin and a winch. The W-3U-1 Alligator was proposed for
the anti-submarine role, but the planned W-3 Sokol-Long, with a
stretch fuselage seating up to 14 fully armed troops, was
discontinued in 1993.
W-3s have
been fitted with several different weapons, including AT-6 Spiral
anti-tank and SA-7 Grail anti-aircraft missiles, 20-mm and 23-mm
cannon, and rocket launchers. At one stage, the manufacturer teamed
with Kentron of South Africa to offer an export version with weapons
systems similar to those of the
Denel AH-2 Rooivalk, but the partnership
failed in 1994.
In its basic
transport form, the W-3 has removable seats and can be used to carry
cargo or casualties as an alternative to passengers. Only one
example of the armed W-3 Huzar has been completed, but development
is continuing.
|