Single-engine rate-of-climb is 410 fpm at full gross, and cabin pressurization differential is the same as the Solitaire. The Marquise, which is 6 feet 2 inches longer, is powered by two turboprops, each producing 778- shp for takeoff or maximum continuous operation and 738 shp at recommended cruise power. With a cabin pressurization differential of 6.0 psi, a sea-level cabin can be maintained up to 14,000. Each engine turns a Hartzell 98-inch four-blade prop and provides a 475-fpm single-engine rate of climb when loaded to full gross. The Solitaire is powered by two turboprops producing 727 shp at maximum continuous power or 689 shp at recommended cruise power of 96% RPM. The MU-2L and MU-2M were discontinued in 1976 and replaced by the MU2N and MU-2P, which evolved into the Solitaire (standard fuselage) and Marquise (stretched fuselage), respectively. Its counterpart, the MU-2M, is a continuation of the Model K. The MU-2L is powered by 776-shp Garrett AiResearch turboprops and carries nine passengers. In 1972, Models J and K were added to the line, both utilizing 724-shp turboprops and offering seating arrangements that corresponded to Models F and G, respectively. The Model F represented a boost in power to 705 shp, and the Model G featured increased seating capacity for up to 11 people. Models B and D were powered by 605 shp and seated 7-9 passengers. The MU-2 is unusual in that it is one of the few high-wing turboprops. The Japanese manufacturer, Mitsubishi, made highly successful aircraft of its own design and of the designs of United States plane makers. Before the earlier versions of the MU-2 had established a substantial penetration of the United States market, certain features of the aircraft were modified to make it more suitable and competitive. Much of this outstanding performance apparently is the result of rather compact overall dimensions for a turboprop twin.
The Mitsubishi MU-2 is a high-performance turboprop with an extraordinary top speed of 370 mph. Engines two 778-shp AiResearch turboprops. Engines two 727-shp AiResearch turboprops. Engines two 724-shp AiResearch turboprops. Engines two 715-shp AiResearch turboprops. See the Master of Music website for concentration-specific submission requirements.STANDARD DATA: (MU-2L) Seats 6-14. The Master of Music program offers concentrations in Composition, Performance, History and Literature, Conducting, and Music Education.
The thesis can be a written project, a recital, or a conducting practicum. Courses within the Woodring College of Education are permissible, as well. Ensembles and studio instruction are also available. The music education concentration includes courses in music education, music history, and music theory courses.
Ensembles and studio instruction are also available. The conducting concentration includes course work in conducting, music history, and music theory, and a conducting practicum to fulfill the thesis requirement. Pianists may emphasize solo performance, pedagogy, or accompanying. The performance concentration includes vocal or instrumental studio instruction, work with small and large ensembles, and course work in music history and music theory. The music history and literature concentration includes seminars in music history, work in notation, courses in music theory, performance (including the Collegium Musicum), and a written thesis. Ensembles, studio instruction, and course work in conducting are also available. The composition concentration includes course work in composition, music history, and music theory as well as a thesis (original composition). Minimum credits for each concentration is 45. The degree may be used as a preparation for doctoral studies in music, or it may serve as a terminal degree. The Master of Music degree consists of a core of courses which serve as a common foundation and a set of more specialized courses in one of five concentrations: composition, music history and literature, performance, conducting, and music education.
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