THE MoTIS E-GRESSOR SERIES IS NOW UNDER DEVELOPMENT
TURBOFANS TURBOJETS TURBOPROPS RAM JETS AFTER BURNERS ENGINE PARTS VTOL ENGINES
MPL PROGRAM INTRODUCTION
Welcome to the MPL-MoTIS PROPULSION LABS. This website is designed to report on the on going testing of the neo-concept MoTIS created jets, rocket , and engine propulsion technologies that the design engineers are testing and are working on behind the scenes at MoTIS VJD (Virtually speaking)..
THE NEW SAMPLE TM-TJ 98-674A UNDER DEVELOPMENT
Super notice: This engine technology is virtual and the sole copyright of team MoTIS and her development staff. We do not copy real world designs at all and strive for excellence in the total design and development of our own stated designs!
FULL DATA COMING!
The analytical and theoretical department
This department will be the most extensive as it will house the true virtual engineering standards on the theoretical possibility of our designs! we will be previewing NASA provided analysis screen shots of engine and rocket dynamics and also exacting scientific data as proof of concepts for our designs. This is more for the engineering specialist and less for the simulation value as we are college educated designers using these programs but all data is for anyone so we are not striving for simplicity but ultra reality..
THE TM 26 TEST TRIALS ARE FINALLY COMPLETE VIEW REPORT NOW!!!
The MPL is not just a research lab but also a teaching facility and a VA analytical test plant of sorts. The goal of the MPL is to design , test , and copyright all sorts of wild designs that will be used in our neo concept aircraft. None of the designs that we work on will in anyway copy real world designs on the drawing board but with follow all real world possibilities in keeping with our reality based neo concept aircraft designs.
The department consists of a CAD design board, a Research and testing lab, and a virtual flying lab.. Each area will handle a different aspect of testing aircraft design concepts using the MSFS/ X-PLANE environments. We for the first time in MoTIS history will be using a real world aircraft model(Virtually speaking) to simulate our jet testing program! The Tu 334 has been chosen to conduct the flight lab testing of our theoretical concept jet and thrust propulsion systems. The aircraft was chosen for its simplicity and easy of loading and off loading of neo concept design components to the base aircraft model. This will be the only real world addition to our concept fleet that will be used as it has some of the easy operations capabilities of the 737-200 series and would have low operating costs. The aircraft engine systems will be switched out testing new systems and engine control units (i.e.. the aircraft will be come known as a concept engine variant system). The name of our test aircraft is being called: PETE-aka. Percussion Engine Transition Equipment.
The first neo concept engine system that we have strapped to PETE is the THRUST MASTER 26LT.
This engines being tested on PETE on the aircraft below represent the replaced engines on for this airframe that are not the original power plants.
The engine design and potential market.
The THRUST MASTER 26LT is a neo concept engine designed by O Watson and William Leclair to be a concept replacement for current turbofan engines on our aging jet fleet. The MSFS programs along with the X-PLANE systems allow us to test the possibilities of our concept systems with out spending millions of dollars in R and D. MoTIS staff is also working on a full C++ testing tunnel to run all our testing concepts in. The specs on the TM 26LT will be released soon but for now the goal of our department is to build the complete engine system as we have done. This is a full MSFS internal combustion design with all animated parts and full opening and observations for the would be mechanic using the engine to simulated maintenance operations! All concept engines will come with new sounds to match their material compositions and vibration characteristics!
TM 26 LT fitted to PETE and shows full internal moving animations and engine heat dynamics!
ENTER TURBOFAN ENGINE TECHNOLOGY (TM 30 X2 LIPT) #2
Note: The EXCEL AERODYNAMICS TESTING labs are very extensive to say the least and this is a sample of test presentations graphics as we will be using this department as a full proof of concept test bed platform as our aircraft are not aesthetic presentations only, but by all real world testing standards must prove in a full released report with profession POH that they can fly, or we wont design them
Terms & Conditions
photos ,logos ,Trademarks, and designs are the sole property of the
MoTIS Industries. We (MoTIS VJD) are a full fledge third party FS
business and not a VA in structure or function. While we use
simulations to test and prove certain neo concept ideas we in no way are
just a MSFS/ XPLANE flight simulations function but exist beyond the
world of simulations as an applications division using simulations to
test theoretical or concept ideas for MoTIS copyright and patent uses.
Title 17 U.S. Code offers protection to the authors of "original works of authorship", including literary, dramatic, musical, artistic, and certain other intellect
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