Tuesday, 10. May 2005 08:07 AM -0400

MoTIS INDUSTRIES NEO CONCEPT AIRCRAFT PREVIEWS

UNDER INTENSIVE REDESIGN


The MoTIS JAVALON is slated to be the flag ship of the MoTIS mass passenger transport mission. This aircraft, along with the Gigantor, Lancet, Mammoth, and soon the MoTIS Sun Runner will comprise the base of the MoTIS airliner infrastructure. We were not kidding years ago when we said that we have a long way to go to execute the base of our development mission as in order to make every thing work right ,we had to build the base infrastructure and the aircraft and departments to support our long range design agenda.

The JAVALON is a medium range passenger aircraft designed for standard altitude flying and moderate speed. This aircraft is still in the data and testing stage at the MoTIS aerodynamics testing labs and we are going to make every attempt to get this aircraft right so please don't expect to see her at your airport until we get her perfectly tweaked!

PROTOTYPE AC#110-22345-7869-010 COMING SOON

This aircraft is the sole design work of O WATSON and J. Guess is handling the project management personally. The JAVALON can fill the range requirements of many aircraft in our current ageing fleets such as the 727's and 737's over the course of the next ten years. The JAVALON is designed with spacious interiors and has decent cargos storage areas. MORE DETAILED DATA AND HISTORY COMING SOON!

This aircraft being previewed in this report is testing some different flight control design configurations, in the negative dihedral elevator placements and the high wing incidence and positive dihedral on the main win for increased lateral stability. this aircraft is planned for a few flavors in the MCT-J2X-A, B, C and the military version. It is much to early to say how far we will expand the variant s of this aircraft ,as each aircraft behaves different in a standard market so only time will tell on how we will expand this aircraft based on its market potential. 

The first test flight of the JAVALON was very rough it needs major flight testing and tuning.

PROTOTYPE AC#110-22345-7869-008


AIRCRAFT DATA AND SPECS COMING

DIMENSIONS    
Span    
Length    
Height    
Fuselage diameter    
Tailplane span    
Cabin length    
Wing area    
Aspect ratio 8  
WEIGHTS, LOADINGS    
Max. take-off weight    
Empty weight    
Fuel weight    
Max. wing loading    
POWERPLANT    
Total take-off thrust    
Thrust loading    
SPEEDS    
Max. cruise speed SL (FL360)    
Best cruise speed (FL360)    
Stall speed (power off, flaps down) (VSC)    
TAKE-OFF (ISA, SL)    
Ground roll    
Obstacle clearance 15m / 50ft    
LANDING (ISA, SL)    
Obstacle clearance 15m / 50ft    
Ground roll    
CLIMB AND ALTITUDE    
Sea level    
Engine out (SL)    
Service ceiling (FAR limit is 25000ft)    
Time to climb to 11000 m / 36000 ft    
RANGES    
Range at best cruise (45 min res.)    
Maximum range    

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

--THIS IS NOT THE FINAL PRODUCT/STILL UNDER INTENSIVE DEVELOPMENT AND TESTING!-- 


IMPORTANT NOTICE: Please be aware that our mission, while channeled and expressed into the dynamic world of flight simulations, is no longer exclusively linked to it, nor are we using flight simulations for pure entertainment value. Thank you.

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"

Important note: Don't be fooled! If you see these aircraft any where else then the reproducers are in direct copyright or patent violation of our intellectual property.

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.

Title 17 U.S. Code offers protection to the authors of "original works of authorship", including literary, dramatic, musical, artistic, and certain other intellectual works. This protection is afforded to both published and unpublished works.

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

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