VIRTUAL FLIGHT LABS ▪  PROPULSION LABS THEORETICAL AERODYNAMICS   MoTIS SCIENCE LAB   NEO CONCEPT FLIGHT PROFILES

TO. V SPEEDS VX/VY TESTING GRD HANDLING TO/ DYNAMICS RANGE TESTING GLIDE TESTING
CRITICAL LIMITS WING DYNAMICS WING LOADING  WEIGHT/BALANCE STALL TESTING STRESS LIMITS
CROSS WIND TESTS AC/ CHARTS  WEATHER TESTING CRASH TESTING ENGINE DRILLS ENGINE TESTS
TAXI TESTS ENGINE OUT TESTS MACH TESTING FIRE TESTING ATTITUDE RECOVERY GEAR TESTING

We have waited for a long time to get down to business in this department! This wing is part of the MoTIS EXCEL FLIGHT LAB! You are about to see the how's and whys of why we design an aircraft! From V speed data gathering , to full range and endurance testing with full calculus equations and all! Get ready to learn tons as we show you how we do it MoTIS style!

M100 VX/VY TESTING

TODAY'S BETA TESTING WAS CONDUCTED BY WILD WILLY BILLY L!

 

Terms & Conditions
All the 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

Copyright (C) 2002, 2003,2004 ,2005, 2006 by MoTIS INDUSTRIES. All rights reserved.

From simulation to reality-Flight in a different direction!

CONTACT US HOME DISCLAIMER

1 1 1

1