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you spend time explaining about obvious parts as cut the foam but not the useful one: Were get this device that goes with de capacitor, or de serial code for it
This is a simple circuit no code a super capacitor 2.7v 10f with charging plug and 750 resister add negative terminal of the capacitor when the capacitor charge with external battery this charging plug work like push button when we remove charging pin it supply current to motor and the capacitor discharge slowly passing out from resistor and the super capacitor capability to charge in short time but dicharge taking time depends on capacitor Farads and Voltage
044 stabs should be made as LIGHT as possible, without reducing their function.! stab root chords should be roughly equal to 2/3 of the wing chord. a couple degrees of SWEEP should be used at the horiz-stab le.! 105 the height of the vert-stab should be equal to a bit less-than 1/2 of the horiz-stab span. 407 you are locating the Center of Mass (c-m); not the cg.! the location of the c-m SHOULD be at a point that vertically aligns with 25 percent of chord. googletranslate
414, 640 the stabs should be optimally designed, so that they are effective And as Light as possible. the length of the common stab root chord should be equal to about 2/3 of the main wing chord. the vert-stab leading edge should be at a slope of 75 degrees. it is not clear whether the profile of the horiz-stab is symmetrical. 426 the fuselage Could be made of pine or spruce or clear-grained poplar. ideally, the (dom of the) fuselage Should be Tapered. the cg should be located at THIRTY percent of chord. this statement assumes that a model airplane has a NORMAL dom. distribution of mass. thirty percent is not a division by three; it is a Multiplication by point-three. googletranslate
