Sunday, 22. October 2006 10:53 AM -0400


THE MoTIS MGAF GA1 AERO FLEX as she is called is one of the first of our Difcraft aircraft fresh out of the design shop! This aircraft is a favorite of the MoTIS designers and we are very proud of this little wonder! This aircraft also coined the BEE TAIL , because of its obliquely shaped nose, like a bees tail, is a true Difcraft as this design takes into consideration three fundamental preexisting aircraft designs concepts. The Gyro plane, the Hang glider, and the Lift body data  from real world NASA lifting body research .(From the days of lifting body test flights-( Data site here- NASA LIFTING BODIES).  This aircraft use what MoTIS CAD designs are calling the VARIABLE PITCH VERTICAL MOUNTED HANG LIFTING BODY WING!- VPMHLW (All designed and developed by team MoTIS AS VIRTUAL TECHNOLOGY!)- All rights reserved.


This aircraft is the sole design work of virtual neo concept design pioneer O. WATSON and J .Guess as its primary designers and numerous student contributions went into making this Difcraft FSReality potential high enough to express it in our favorite FS programs as a potential new aviation concept (THE VPMHLW that is)... The development of the flight model was trying to say the least and she is still some what unstable! Its like mounting a composite semi ridged hang gliding wing onto a fat nosed (designed that way for center of gravity range reasons) composite trike that is the size of a piper warrior! (Surface area especially!) The AERO FLEX is so very light in construction due to the modern composite techniques! This aircrafts skin is so light and strong that we are giving it a virtual test thickness of only 1.2 inches in diameter.


The panel is of a new ergonomically constructed design that has an integrated 2 way MDF in the central console as well as two PFD units that are laved out in numerically expressed digital flight performance values. This is considered a high quality MoTIS neo concept panel design.



SWING LIFTING- Torque swinging the lifting body wing against the alternating CG position and moments against the moving lift vectoring wing and the thrust vectoring engine moments! (If you are not a big aerodynamics design buff-THAT TRANSLATES INTO A LOT OF LIFT, a super low stall speed, a awesomely slow flying plane at minor and major critical AOA's and (If we can keep it stable and in good CG range limits and super full reduction in forward cruising speeds-which are low any how as she is just a small craft by weight in the prototype testing phase), and as all aircraft function in the transportation business in some capacity-larger carrying loads if we develop her further into a passenger/cargo aircraft of some type. Hint... ..


This aircraft will have major takeoff and landing advantages do to the ultra high angles of attach that can be attained on take off and landings- The LEV wing its self easily moving 32 Degrees in standard maximum deflection!!! The neo concept is actually very sound its the weight and balance/ lift stability issue that makes this design so exciting and conversely so challenging! The wing of choice for this aircraft Difcraft is called the LEVARC 2500. This wing array has a rounder leading edge and wing warping elevatorlets and aleronlets that auto warp to meet the demands of changing lift requirements at different AOA's

The aircraft can be configured to carry larger surface area LEVARC LIFTING BODY WINGS ALSO!


Note: All of these concept aircraft are from the design staff of the MoTIS CAD engineering board and our CEO. We do not copy others work or design real world concept aircraft at all. Each of our aircraft are from our heads and are the sole intellectual property of MoTIS and we can prove it. We take great pride in all of our true concept designs and do not create real world aircraft, model aircraft variants or concepts, or other designers concept work at all ,but stand by our mission statement in truly creating "OUR OWN DESIGNS"

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 a real world applications division using simulations to test theoretical or concept ideas for MoTIS copyright and patent uses.