WSK SO-3

SO-1/SO-3
SO-1 engine on display at the Polish Aviation Museum
Type Turbojet
National origin Poland
Manufacturer WSK PZL Rzeszów
First run November 1948
Major applications PZL TS-11 Iskra
Number built 580


The WSK SO-1 and WSK-SO-3 are Polish turbojet engines designed by the Instytut Lotnictwa (Institute of Aeronautics ) and manufactured by WSK PZL Rzeszów, to power the PZL TS-11 Iskra jet trainer. Thirty SO-1s were built, this being superseded by the improved SO-3, of which a further 580 were built.[1] The engine has a seven-stage compressor, annular combustion chambers, and a single-stage turbine.

Variants

SO-1
Original production. Overhaul life 200 hours.[2]
SO-3
Improved version of SO-3, intended for tropical use. Modified compressor, combustion chamber and turbine.[2] Overhaul life 400 hours.[3]
SO-3W22
Modified version for PZL I-22 Iryda, 10.79 kN (2,425 lbf) rating, renamed PZL-5.[4]

Applications

Specifications (SO-3)

Compressor intake

Data from Jane's All The World's Aircraft 1988-89.[2]

General characteristics

Components

Performance

See also


Comparable engines
Related lists

References

Wikimedia Commons has media related to WSK SO-3.
  1. Lambert 1993, p.630.
  2. 1 2 3 Taylor 1988, p.699.
  3. http://www.amw.com.pl/zos_product_info.php?zos_products_id=59
  4. Taylor 1996, p.572.
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