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112     Bu il d  Y o ur  O w n  Q u a d c o p t e r























                             Figure 5.25  Chart of power versus propeller r/min.


                             propeller at 7000 r/min. 150 W would mean that approximately 12.3 A would be needed at
                             a 12.2-V battery-supply voltage. I would estimate that 7000 r/min would be the maximum
                             rotational speed for the particular propellers used in the Elev-8. The following calculation
                             shows you how to determine the maximum flight time using 100% power:
                                 One motor/propeller combination at 7000 r/min = 12.2 A
                                 Four motor/propellers at 7000 r/min = 12.2 × 4 = 48.8 A
                                 Using the 3S LiPo battery discussed in Chapter 3 = 4200 mAh = 4.2 Ah
                                 Maximum time at 7000 r/min = 4.2/48.8 × 60 min = 5.16 min

                                Wow! Only about 5 minutes at maximum power is a startling fact for quadcopter
                             operations. Operating times can be extended by using higher-capacity batteries, but that
                             comes at a cost of reducing the effective payload capacity, since using bigger batteries means
                             heavier batteries. The other preferred way of extending operating times is to operate at
                             much lower r/min settings. I created Table 5.4 to show estimated operating times and thrust
                             versus r/min for the battery described above.
                                Table 5.4 shows how the propeller speed affects both time and the creation of thrust. It is
                             definitely  a  tradeoff  that  you  have  to  consider  constantly  while  you  are  operating  the


                                           Power     Voltage  Amperage   Time    Thrust   Total Thrust
                                 r/min     (w)       (V DC)   (A)        (min)   (grams)  (grams)
                                 0         0         12.56    0.02       n/a     n/a      n/a
                                 1140      3         12.56    0.24       263.8   50       200
                                 3450      20        12.53    1.60       39.5    168      672
                                 4710      51        12.44    4.10       15.4    343      1372
                                 6030      103       12.35    8.34       7.6     631      2524
                                 7000      150       12.20    12.3       5.1     860      3440

                                Table 5.4  Thrust and Time versus r/min
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