Test Run of 120kgf Thrust gas Turbine Engine for UAVs by Kalyani

Опубликовано: 14 Октябрь 2024
на канале: Defence Decode

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Kalyani's KCTI 120...
120kgf Thrust gas Turbine Engine.
Technology realized.

Specifics:
Cross over diffuser
Reverse-flow combustor with Effusion cooling.
3D print Flame tube.
• 2.2 Kg/sec Mass Flow Rate
• 55,000 RPM (Max)
• ~25kg in Overall Weight

Applications
UAV
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SOURCE► #DefenceDecode #KCTI
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