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 THRUST MASTER VIRTUAL ENGINE TECHNOLOGY


TURBOFANS Thrust Range: 26-86,000 LBS TM 26   TM-36+  TM-66  TM-86

Thrust Range: 32-36,000 LBS

 

 

SPECIALTY TURBOFANS Thrust Range: 86,000-HIGHER! LBS TM-TJ 98-674A  TM-TJ 39AB41   MPL TM-30 X2 LIPT

PISTON Thrust Range: COMING...

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.

  MoTIS  2002, 2003,2004 ,2005, 2006, 2007, 2008 by MoTIS INDUSTRIES. All rights reserved.

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