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!