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MoTIS M CLASS M100- ENGINES


TM 32-36 ENGINE SPEC DATA COMING:

Max Diameter (Inches):  Length (Inches):
Dry Weight (Lb.): 
First test flight:
Engine weight:  Thrust:
Maximum altitude:

Note: All engine thrust rating are with in MoTIS VJD aircraft needed propulsion values for providing actual and calculated thrust @SL for all our standard and aerodynamics certified airframes. All MoTIS neo concept engine systems follow the standard design process of  intake. Compression, Combustion, and Exhaust and can be verified and proved by MoTIS mathematical calculations that these engines can be built and are on the paper drawing board for real world patent consideration. . All engine designs are the sole intellectual property of the MoTIS INDUSTRIES design staff and are not the copyrighted property of any aerospace division other then the MoTIS virtual design laboratories. We take great pride in the total creation and testing and implementation of what we have always called" Our own design", and will continue to create never before seen neo concept designs and protect the rights, marks , and patents of our intellectual property.