Tennessee University Offers Online MBA program Essays

Tennessee University Offers Online MBA program Essays Tennessee University Offers Online MBA program Essay Tennessee University Offers Online MBA program Essay Essay Topic: Toefl Tennessee University in Chattanooga, a public university, has online MBA programs and the deadline for applying is progressing. Tennessee University records all of the online classes and archives them for further use. The Association to Advance Collegiate Schools of Business represents the gold standards of accreditation for business schools and the online MBA program at Tennessee University is accredited by it. The online business graduate program at Tennessee University was founded in the academic year 2013-2014. The registration deadline is progressing so if you think on applying for this program, you should do that as soon as possible. The application deadline is the same for in-state US residents and out-of-state international students. The director of admissions is Bonny Clark and the telephone number for more information on admissions is 423 425 4667. Tennessee University awards MBAs and the degree can be earned online. The recommended Internet speed for this online MBA program is Cable Internet speed. There is an instructor who will respond to any calls and he/she is available 24 hours. The part-time tuition for this online business graduate program at Tennessee University for in-state US residents is $700 and the part-time tuition for out-of-state international students is $744. As mentioned above, the deadline for applying for this online program is in progress and the notifications for admission start arriving from November 1st. It is possible for the university to deny the application of some applicants that are qualified for the program. It is important to note that the university accepts admissions from people who live abroad. Also, the program is not an SOC member and it does not offer DANTES courses. For applying, an application essay is required and the tests that are required are GMAT or GRE. Applicants must have 2 letters of recommendation and 2 letters of recommendation coming from their professional contacts. Also, the applicant must have work experience in the business area and an undergraduate degree from a business-related field. Undergraduate coursework is not required. Besides GRE and GMAT, international students have to take a TOEFL test as well and the minimum score they need for the paper-based test is 550 and for the Internet-based test the score they need is 79. The academic factors that are considered in the application process are the undergraduate institution the student comes from, the class rank and the undergraduate field of study the student has chosen. The undergraduate GPA, the test scores and the recommendation letters are very important and represent a deciding factor. From the non-academic factors, the most important are the application essay, the previous work experience the student has and the interest the applicant shows for this program. The interview is also a factor that is considered as well as the personal characteristics the applicant owns. Being a student of the generation is not a deciding factor for getting admitted for the program. Director of admissions at Tennessee University is Bonny Clark. The contact telephone for getting information about admissions and the application process is 423 425 4667.

The Bell X-1 and Breaking the Sound Barrier

The Bell X-1 and Breaking the Sound Barrier Bell X-1E Specifications: General Length: 31 ft. Wingspan: 22 ft. 10 in. Height: 10 ft. 10 in. Wing Area: 115 sq. ft. Empty Weight: 6,850 lbs. Loaded Weight: 14,750 lbs. Crew: 1 Performance Power Plant: 1 Ãâ€" Reaction Motors RMI LR-8-RM-5 rocket, 6,000 lbf Range: 4 minutes, 45 seconds Max Speed: 1,450 mph Ceiling: 90,000 ft. Bell X-1 Design Development: Development of the Bell X-1 began in the waning days of World War II as the interest in transonic flight increased. Initially contacted by the US Army Air Force and the National Advisory Committee for Aeronautics (NACA - now NASA) on March 16, 1945, Bell Aircraft began designing an experimental aircraft dubbed the XS-1 (Experimental, Supersonic). In seeking inspiration for their new aircraft, the engineers at Bell elected use a shape similar to a Browning .50-caliber bullet. This was done as it was known that this round was stable in supersonic flight. Pressing forward, they added short, highly-reinforced wings as well as a movable horizontal tailplane. This latter feature was included to give the pilot increased control at high speeds and later became a standard feature on American aircraft capable of transonic speeds. In the interest of retaining the sleek, bullet shape, Bells designers elected to use a sloped windscreen in lieu of a more traditional canopy. As a result, the pilot entered and exited the aircraft through a hatch in the side. To power the aircraft, Bell selected an XLR-11 rocket engine capable of around 4-5 minutes of powered flight. Bell X-1 Program: Never intended for production, Bell constructed three X-1s for the USAAF and NACA. The first began glide flights over Pinecastle Army Airfield on January 25, 1946. Flown by Bells chief test pilot, Jack Woolams, the aircraft made nine glide flights before being returned to Bell for modifications. Following Woolams death during practice for the National Air Races, the X-1 moved to Muroc Army Air Field (Edwards Air Force Base) to begin powered test flights. As the X-1 was not capable of taking off on its own, it was carried aloft by a modified B-29 Superfortress. With Bell test pilot Chalmers Slick Goodlin at the controls, the X-1 made 26 flights between September 1946 and June 1947. During these tests, Bell took a very conservative approach, only increasing speed by 0.02 Mach per flight. Dismayed by Bells slow progress towards breaking the sound barrier, the USAAF took over the program on June 24, 1947, after Goodlin demanded a $150,000 bonus for achieving Mach 1 and hazard pay for every second spent over 0.85 Mach. Removing Goodlin, the Army Air Force Flight Test Division assigned Captain Charles Chuck Yeager to the project. Familiarizing himself with the aircraft Yeager made several test flights in the X-1 and steadily pushed the aircraft towards the sound barrier. On October 14, 1947, less than a month after the US Air Force became a separate service, Yeager broke the sound barrier while flying X-1-1 (serial #46-062). Dubbing his plane Glamorous Glennis in honor of his wife, Yeager achieved a speed of Mach 1.06 (807.2 mph) at 43,000 feet. A publicity boon for the new service, Yeager, Larry Bell (Bell Aircraft), and John Stack (NACA) were awarded with the 1947 Collier Trophy by the National Aeronautics Association. Yeager continued with the program and made 28 more flights in Glamorous Glennis. The most notable of these was on March 26, 1948, when he reached a speed of Mach 1.45 (957 mph). With the success of the X-1 program, the USAF worked with Bell to build modified versions of the aircraft. The first of these, the X-1A, was intended to test aerodynamic phenomena at speeds above Mach 2. First flying in 1953, Yeager piloted one to a new record speed of Mach 2.44 (1,620 mph) on December 12 of that year. This flight broke the mark (Mach 2.005) set by Scott Crossfield in the Douglas Skyrocket on November 20. In 1954, the X-1B began flight testing. Similar to the X-1A, the B variant possessed a modified wing and was used for high speed testing until it was turned over to NACA. In this new role, it was used until 1958. Among the technology tested on the X-1B was a directional rocket system that was later incorporated into the X-15. Designs were created for the X-1C and X-1D, however the former was never built and the latter, meant for use in heat transfer research, only made one flight. The first radical change to the X-1 design came with the creation of the X-1E. Constructed from one of the original X-1s, the X-1E featured a knife-edge windscreen, new fuel system, a re-profiled wing, and enhanced data collection equipment. First flying in 1955, with USAF test pilot Joe Walker at the controls, the aircraft flew until 1958. During its final five flights it was piloted by NACA research pilot John B. McKay who was attempting to break Mach 3. The grounding of the X-1E in November 1958, brought the X-1 program to a close. In its thirteen-year history, the X-1 program developed the procedures that would be used in subsequent X-craft projects as well as the new US space program. Selected Sources NASA: Bell X-1 National Air Space Museum: Bell X-1