M-DOT AEROSPACE Has a Complete Stand-Alone Engineering Department Specializing In:

design of small gas turbines and turbomachinery including -

Under US Government (DARPA, Army, Navy and Air Force) funding, we have internally developed a 94 horsepower twin spool turboprop for uav propulsion called the TPR80. The engine design can be produced in recuperated and non-recuperated form. We are currently developing a micro turbine engine under DARPA funding that will propel micro-air vehicles ( mav s). This engine can be configured as a variety of turbomachines including microturbojet, turboprop and turboshaft. Call or e-mail us today to quote your engine design program needs.

gas turbine engine components and systems including -

Through our participation in government and commercially funded development programs, we have developed expertise in structural design and aerodynamic design of centrifugal compressors, axial fans and compressors, annular and can-type combustors and burners, radial inflow turbines and axial turbines, turbine castings, impeller castings, high speed gearboxes and fluid pumps. We have also developed a specialization in microturbines, microcompressors and tiny burners. Our capable engineers are experienced in aerodynamics, foil bearings, shaft dynamics, stress analysis, and cycle thermodynamics. We are conducting research in the fields of ultra high speed turbine, alternator and electric motor development achieving speeds in excess of 500,000 rpm. Our goal is to reach a million rpm in a microturbine, motor or alternator

Other turbomachines and systems including -

We have produced and successfully tested a tiny jet-fuel turbopump for the Navy capable of achieving 1300 psi output pressure at roughly 100,000 rpm. We have designed and fabricated a noise suppressing exhaust system for an APU that reduced back pressure yielding a remarkable increase in power.

We Also Specialize In:

complex prototypes and laboratory systems including