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The aircraft was designed for private and club use and served as a trainer and glider tug. Heini
Dittmar, the aircraft’s designer, was killed in 1960 when his Motor-Möwe crashed near Essen/Mulheim airport. Small numbers of the type were completed by the end of 1960 and on 1 January 1961 four HD 153
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sailplane, was a motorized development of this sailplane and was initially designed to be powered by engines of 48–63 kW (65–85 hp). The HD 153 prototype was a two-seat side-by-side high wing monoplane powered by a 48 kW (65 hp)
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and four HD 156 Motor–Möwen appeared in the West German civil aircraft register. I 1965 four HD 153 and five HD 156 Motor-Möwen were registered in West
Germany. By 2007, no examples were known to be active.
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engine and was of wooden construction with detachable wing and tail assemblies to facilitate road transportation when needed. A second prototype aircraft was fitted with a 45 kW (60 hp)
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140 L (36.98 US gal; 30.80 imp gal) in two wing tanks + optional 200 L (52.83 US gal; 43.99 imp gal) overload tank
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HD 156 three-seat aircraft showing the revised front and side cabin glazing of this model.
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4-cylinder air-cooled horizontally-opposed piston engine, 67 kW (90 hp)
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478:. London: Jane's All the World's Aircraft Publishing Co. Ltd. p. 175.
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11-APR-1959 wing separated during descent after glider towing
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463:. London: Macdonald & Co. (Publishers) Ltd. p. 73.
433:. London: Macdonald & Co. (Publishers) Ltd. p. 65.
418:(in German). München: AFRO-Verlag Hubert Zuerl. p. 57.
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three-seat aircraft fitted with additional side windows
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2-bladed
Hoffman "HoCo" fixed pitch wooden propeller
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World
Aviation Register - West Germany 1961 edition
250:one passenger (334 kg (736 lb) payload)
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366:1,872 km (1,163 mi, 1,011 nmi)
515:28-APR-1960 Heini Dittmars fatal test flight
459:Green, William; Pollinger, Gerald (1965).
429:Green, William; Pollinger, Gerald (1955).
44:HD 153A-1 Motor-Möwe two-seat aircraft at
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384:1,000 m (3,300 ft) in 6 minutes
360:1,000 km (620 mi, 540 nmi)
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347:150 km/h (93 mph, 81 kn)
341:170 km/h (110 mph, 92 kn)
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476:Jane's All the World's Aircraft 1958-59
372:4.5 hours (13 hours with overload tank)
230:Jane's All the World's Aircraft 1958-59
223:Specifications (HD 153 with C90 engine)
148:that was first flown in November 1953.
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354:65 km/h (40 mph; 35 kn)
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298:465 kg (1,025 lb) equipped
119:private pilot owners and aero clubs
535:1950s German civil utility aircraft
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274:18.3 m (197 sq ft)
268:2.1 m (6 ft 11 in)
256:6.5 m (21 ft 4 in)
262:12 m (39 ft 4 in)
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545:Single-engined tractor aircraft
474:Bridgman, Leonard, ed. (1957).
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496:"Dittmar HD 153 Motor-Möwe".
448:. Acton, London: Air-Britain.
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378:4,500 m (14,800 ft)
550:Aircraft first flown in 1953
156:The Motor-Möwe, designed by
56:Light civil utility aircraft
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304:760 kg (1,676 lb)
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461:The Aircraft of the World
431:The Aircraft of the World
416:Dittmar H. D. - 53 "Möwe"
139:Dittmar HD 153 Motor-Möwe
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18:Dittmar HD-153 Motor-Möwe
396:130 m (427 ft)
390:150 m (492 ft)
235:General characteristics
414:ZUERL, HUBERT (1954).
292:Göttingen 367 modified
208:production two-seaters
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152:Design and development
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160:who had designed the
318:Continental C90-12F
177:Operational history
540:High-wing aircraft
202:two-seat aircraft
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162:Dittmar HD 53 Möwe
130:Dittmar HD 53 Möwe
116:Primary user
30:HD 153 Motor-Möwe
382:Time to altitude:
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332:Performance
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143:West German
529:Categories
401:References
370:Endurance:
272:Wing area:
260:Wingspan:
248:Capacity:
228:Data from
205:HD 153A-1
82:Designer
186:Variants
173:engine.
77:Dittmar
48:in 1965
288:Airfoil
266:Height:
254:Length:
108:Status
358:Range:
215:HD 156
199:HD 153
141:was a
242:Crew:
171:Hirth
103:1956
53:Role
316:1 ×
137:The
283:8.5
244:one
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