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Gas turbine engine NK-16ST

Description

Longitudinal section of NK-16ST aircraft gas turbine engine with technical characteristic and specification Technical characteristic Rated power _ 16000 kW Rotor speed: high pressure __ 6900 rpm low pressure ___ 5270 rpm free turbine _ 5300 rpm Mass _____________ 7800 kg

Project's Content

icon gazoturbinnyy-dvigatel-nk-16st.cdw
The material is a file that can be opened in program:
  • Kompas or KOMPAS-3D Viewer

Additional information

Drawings content

icon gazoturbinnyy-dvigatel-nk-16st.cdw

gazoturbinnyy-dvigatel-nk-16st.cdw
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