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design producing 12.5 kW (17 hp) at 1950 rpm, with an outrunner coil. It has a 93% efficiency. The low working rpm of the engine means that it can turn a propeller at efficient speeds without the need for a
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277:, pages 262-263. Flying Pages Europe SARL, 2015.
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275:World Directory of Light Aviation 2015-16
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201:12.5 kW (17 hp) at 1950 rpm
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273:Tacke, Willi; Marino Boric; et al:
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16:German aircraft electric motor
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75:, designed and produced by
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155:3.75 kg (8.3 lb)
317:Aircraft electric engines
149:215 mm (8.5 in)
143:171 mm (6.7 in)
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250:List of aircraft engines
123:General characteristics
112:Specifications (HDP 10)
91:Design and development
218:Power-to-weight ratio
232:Related development
77:Geiger Engineering
56:Geiger Engineering
73:electric aircraft
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33:Electric aircraft
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300:Official website
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211:Best efficiency:
95:The HDP 10 is a
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238:Geiger HDP 13.5
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177:Cooling system:
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136:aircraft engine
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106:reduction drive
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79:of Seigendorf,
41:National origin
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207:58V nominal
193:Performance
153:Dry weight:
85:Oberfranken
256:References
160:Components
283:1368-485X
222:3.3 kW/kg
172:outrunner
147:Diameter:
134:electric
132:Brushless
117:Data from
97:brushless
81:Hirschaid
311:Category
227:See also
205:Voltage:
141:Length:
46:Germany
35:engine
24:HDP 10
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169:type:
129:Type:
119:Tacke
29:Type
279:ISSN
188:none
167:Coil
101:volt
63:The
213:93%
179:air
99:58
313::
264:^
108:.
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83:,
220::
186::
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