MoTIS CABAR CONGO STANDARD CONCEPT ART/SCREEN SHOTS!
Sunday, 02. May 2004
---PROTOTYPE STILL UNDER TESTING- MODEL CABAR CONGO M-1US---
Well designing next generation neo concept aircraft some times means creating all new categories for the great new designs that can serve in many new areas of the flight work environment and the Hyber-Light series of Ultra light/STOL aircraft is no different. The Hyber Light term has been defined and coined by MoTIS CEO O WATSON and applies to our neo concept line of Ultra light? STOL aircraft that are one part ultra light in performance and one part light weight STOL( Short Take off and Landing ) aircraft.
PRIMARY TEST MODEL
As and ultra light is certified as a true single pilot operated light aircraft the Hyber-Light will have to operate under certain Ultra light r4strictions but as a STOL utility aircraft with super low stall speeds this brand of aircraft could reasonable compete with the helicopter minis the ability to hover.
The key to the Hyber-Light aircraft is to design them to stall at speeds under 12kts!!! This would give a Hyber -Light pilot great access to the flight environments of many patrol helicopters allowing them to stay with in a ultra close and safe flying range and radius!
---TEST PILOT WILL BE REPLACED WITH A FACTORY ISSUED PILOT UPON RELEASE---
--FS 2002 snap shot of VC cockpit under construction--
Reasonable forward speeds, low takeoff and landing runs, excellent visibility, super low stall speeds , low operational costs, and the multi mission usages will make the MoTIS defined Hyber-Light a great next generation Ultra light/ STOL aircraft of the future a great work horse for years to come!!
Artistic rendering of the MoTIS CABAR in-flight. Copyright (C) 2004 by MoTIS Virtual Jet Design. All rights reserved
These aircraft can be used in SAR missions, police departments, light utility transport, and for sport and recreational purposes.
Complete Hyber-Light aircraft History coming soon!
The secondary model was designed with a larger rudder area and a tail skid to avoid tail strikes on take off and landing.
----SECONDARY TEST MODEL----
NOTE: Aircraft under serious construction and subject to changes as flight testing ensues.
Prototype model AC#110-22345-7989-001
Length: in --- Wingspan: ft ---Height: ft ---Empty Wt: 1lbs---Wing areasq ft ---Wing Loading: lbs/sq ft ---Engine: NA ---Max Thrust: NA --- V Max hi:--- Ceiling: ---Climb Rate: fpm ---Range: NA
Full Specs Coming soon...
HEAD OVER TO THE FACTORY AND SEE WHAT'S NEW!
"ALL AIRCRAFT CREATED AND DESIGNED FROM SCRATCH BY MoTIS VIRTUAL JET DESIGN!"
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"
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|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.|
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Last modification: Sunday, 02. May 2004 08:48
Copyright (C) 2002,2003, 2004 by MoTIS Virtual Jet Design. All rights reserved