|Wing Load (kg/m2)||278|
|Power load (kg/hp)||3.16kg/kgf|
|Speed at 0m||864km/h|
|Speed at *m||911km/h|
Production aircraft, based on the I-300/F. It differed from prototype by dorsal fin, strengthening the tail structure and improving course stability. Also added were flaps/airbrakes to cut the Landing Roll (it was up to 1060m). To protect tail from the jet exhaust shin steel plate was installed in 15mm from fuselage right after the engine.
With extra fuel tanks takeoff weight was increased by 500kg, range - by 300km and climb to 5000m - from 4.5min to 6.25min. In this configuration MiG-9 was used as an escort fighter.
State trials took place on October 22, 1946 - as was scheduled, without delays.
(39k) MiG-9 at the Monino AF Museum, photo by Paul Nann;
photo (20k) by Ken Duffey, 1993; see more at Monino AF Museum Page maintained by A.Gretchihine;
|Modified October 23, 1997||Back to|