The rotating assembly (shaft, compressor, and turbine wheel) must be balanced to a fraction of a milligram. Standard workshop tools cannot achieve this; specialized dynamic balancing equipment is required.
Are you looking to , or troubleshoot a commercial unit?
If you have acquired the PDF (legally), here is your project roadmap: model jet engines thomas kamps pdf
While early experimental model engines attempted to mimic axial-flow designs (similar to large passenger jets), Kamps recognized that for small-scale models, the centrifugal compressor was superior. His work details the engineering rationale for this choice:
by Thomas Kamps is a seminal technical guide that demystifies the design, construction, and operation of small-scale gas turbines. While physical copies are available through retailers like Sarik Hobbies and Desertcart , digital versions are often hosted for reference on platforms like Internet Archive and Scribd . Core Technical Features The rotating assembly (shaft, compressor, and turbine wheel)
Consult with experienced professionals or join established modeling organizations for hands-on guidance.
Unlike theoretical textbooks, Kamps provides actionable data on: If you have acquired the PDF (legally), here
Thomas Kamps is a German engineer and RC aviation pioneer who played a crucial role in commercializing and documenting miniature gas turbines. Before his work, early model jet pioneers like Kurt Schreckling began experimenting with homemade turbines using crude materials, such as wooden compressors.
Exhaust gas temperatures (EGT) routinely sit between 600°C and 750°C.
When designing model jet engines, several key factors must be considered: