KV (rpm/v) Motor Weight(g) Vottage (V) NO Load Current(A) NO Load Speed (rpm) Load Current (A) Load Speed (rpm) Prop Pull(g) 2000 5 7.4 0.4 8200 2.2 6050 EP7035 85 3000 5 3.7 0.4 11000 2.6 5780 EP6030 50               一. (Application):       Use for indoor plane. Airplane class No about: 50 g (weight).   二. Advise configure and usage limit):      1. Advise application power 16 W      2. Momentary power  20 Wmax      3. Propose configure for this motor:           a. Battery---800 mAh 10 C lipo      b. ESC--- 7A.   c. propeller---EP7035               4. Don′t let the exiguous carbon steel metal to close with motor when fixing, it breathe inside motor by magnetic field then cause the motor to set up or cause the winding short!                   5. Please use the stainless steel screws when fix the motor, and the length of the screw don′t higher than the pedestal, lest to breach the wire!        6. Motor temperature should not exceed 90℃   三.  Configuration characteristic:           1. Magnet---N35SH           2. Silicon steel--- 0.35(mm)           3. Bearing---NMB           4. shaft--- Carbon steel           5. Guide wind system---  Free cooling           6. Insulated material--- Somar Epoxy (Japan)   四. Accessories: Front prop holder、Rear prop holder、Cross motor mount、″L″motor mount、″L″stick motor mount.(See attached drawing )   五. Reliability Testing:       1. Test Condition           a. Voltage---7.4(V)                              b. Propeller---EP7035                             c. Load current---2.2(A)                        d. Net Thrust---85(g)                  e. Room temperature---25(℃)                        f. Run mode---5 Minute ON, 2 Minute OFF           g. Shaft direction gap--- 0.05-0.2mm           h. Noise no load--- 30 db     2. After testing 100 times circle           a. Net thrust---80 (g)                  b. Current--- 2.3 (A)              c. Temperature rising---85 (℃)                d. Shaft direction gap---0.1-0.2mm           e. Run mode---5 Minute ON, 2 Minute OFF