![]() The principal performance in the various configurations is summarized in the following table. The rate of roll is slower, due to the weight being farther from the longitudinal axis of the airplane.Ĭontrol forces are good, but as in the earlier model P-47 airplanes large changes in trim are necessary for a change in airspeed. The P-47 N airplane has performance and handling characteristics very similar to the early P-47 airplanes, but due to heavier weights caused by greater fuel capacity, performance is lower when using equal power settings. Some additional data is included for two combinations of external wing tanks. This report includes pilot’s comments, speed, range, and climb performance at various powers, weight and altitude for the clean airplane. Take-off tests with two 165 gallon wing tanks, one 110 gallon belly tank and ten, five inch rockets. Range Survey through simulated tactical missions. Zoom Characteristics of P-47N-2 airplane AAF No. Take-off and Landing tests on P-47N airplane, AAF No. Performance of P-47N with and without Special Rocket Installations. ![]() Some parts of the original program were cancelled, other portions were completed on other P-47N airplanes and have been reported separately.ġ. The first airplane assigned to this project crashed when approximately half way through the program. Tests to determine angle of attack vs airspeed were also requested by the Armament Laboratory. for seven different drag configurations (bombs, tanks, rockets, etc.). ![]() Stability tests and complete performance tests including take-off, landing, climb, speed and range were originally requested at all power setting from seal level to 40,000 ft. ![]() These tests were requested by the Fighter Branch, Production Engineering Section, Procurement Division, and by the Flight Data Branch of the technical Data Laboratory to check the guaranteed performance and Technical Order 01-65BD-1. Jaskot, of the Fighter Operations Section. During this time 67 hours were flown in 39 flights, by Captain J. Flight tests were run on P-47N airplane, AAF No. The P-47 N was designed as a long range fighter-bomber, differing from other P-47 airplanes in that it has more powerful engine, a new turbo-supercharger, more fuel, an automatic pilot, homing radio and a tail warning radar. ![]()
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