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Balsa USA Enforcer
I got a BalsaUSA Enforcer kit tonight to do as an electric conversion.
http://www.balsausa.com/store/product.php?id_product=47 I'm going to power with a Turnigy something or other and 10S A123's. I'm going to join the 1000watt club finally with this one. I'm going to add mechanical retracts most likely Robart. |
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Quote:
Flew one of those (nitro) a couple decades ago - VERY agile performer. Be sure to keep the main gear short and the nose long - it needs considerable angle of attack to break ground. |
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I haven't posted much but quite a bit more has been done. The fuselage is close to finished except for finishing up the hatch. The bottom sheeting is on the wing and I've got the retract locations planned and just need to trim the ply doublers a bit for the rails. I've got the nosegear location planned. I'm going to mount the nose gear to retract forward into the nose. Looking at the CG I don't think the battery will need to go that far forward so that aren't doesn't need to be preserved for battery space.
I ordered the motor for this tonight. Found an AXI 4130/20 on closeout somewhere for a decent price. http://www.bphobbies.com/view.asp?id...308&pid=AXI111 There really is no bargain out there for speedcontrols that will handle 10S Voltage. I'm going to go with a Castle Creations Phoenix ICE 50amp 33volt. Turnigy controllers and anything else from hobbyking cost nearly as much. http://www3.towerhobbies.com/cgi-bin...&I=LXVJN0&P=SM The ESC's aren't available anywhere at the moment but I don't need the ESC until March or so much later on in construction. I did some work on moto-calc and came up with the following for the motor/battery/prop combo. Going to go with something around a 14x12 APCe prop. Motor: Model Motors AXI AC4130/20; 305rpm/V; 1.2A no-load; 0.099 Ohms. Battery: A123 ANR26650 M1 (30C); 10 cells; 2300mAh @ 3.3V; 0.016 Ohms/cell. Speed Control: Castle Creations Phoenix 80; 0.001 Ohms; High rate. Drive System: 14x12 APC Prop; 14x12 (Pconst=1.17; Tconst=1) direct drive. Airframe: Enforcer; 1080sq.in; 113.3oz RTF; 15.1oz/sq.ft; Cd=0.033; Cl=0; Clopt=0.29; Clmax=0.8. Stats: 126 W/lb in; 100 W/lb out; 22mph stall; 37mph opt @ 51% (24:23, 91°F); 1996ft/min @ 37.9°; -590ft/min @ -10.5°. Warning: MotoCalc was unable to determine a throttle setting for hands-off cruise airspeed, so the best lift-to-drag ratio airspeed and throttle setting will be used instead. Inability to determine a throttle setting for an airspeed usually means the model is not capable of reaching the required speed with the given power system, or the airfoil information has not been specified correctly. Power System Notes: The full-throttle motor current at the best lift-to-drag ratio airspeed (32.8A) falls approximately between the motor's maximum efficiency current (18.3A) and its current at theoretical maximum output (140.6A), thus making effective use of the motor. The voltage (27.8V) exceeds 12V. Be sure the speed control is rated for at least the number of cells specified above. Possible Aerodynamic Problems: The static pitch speed (79mph) is greater than 3 times the stall speed (22mph), which might make take-off or hand launching difficult, and is inefficient in flight unless high speeds are intended. Pitch speed can be decreased by using a lower pitched and/or larger diameter propeller, a higher gear ratio, a lower cell count, or some combination of these methods. The diameter (14.0in) to pitch (12.0in) ratio is less than 1.5:1, which will result in reduced propeller efficiency at low speeds (the propeller is stalled). Although this is not likely to affect flying characteristics, it may make take-off or hand launching difficult. Aerodynamic Notes: With a wing loading of 15.1oz/sq.ft, a model of this size will have very sedate flying characteristics. It will be suitable for relaxed flying, in calm or very light wind conditions. The static thrust (110.4oz) to weight (113.3oz) ratio is 0.97:1, which will result in very short take-off runs, no difficulty taking off from grass surfaces (assuming sufficiently large wheels), and steep climb-outs. At the best lift-to-drag ratio airspeed, the excess-thrust (73.2oz) to weight (113.3oz) ratio is 0.65:1, which will give steep climbs and excellent acceleration. This model should be able to do consecutive loops, and has sufficient in-flight thrust for almost any aerobatic maneuver. General Notes: This analysis is based on calculations that take motor heating effects into account. These calculations are based on mathematical models that may not account for all limitations of the components used. Always consult the power system component manufacturers to ensure that no limits (current, rpm, etc.) are being exceeded. |
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Here are a couple of my electric enforcer based airframes. The single seater was lost a couple seasons back due to bad case of dumb thumbs and out of trim airframe. The twice seater flies just over a hundred miles an hour and is a blast. Based off the Ivan Schomer update for ducted fan. Hacker powered but waiting future update before flying again. Very sweet flying vehicle. ed
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