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Gotha Go 150 - Wikipedia

From Wikipedia, the free encyclopedia

Gotha Go 150

Role	Light aircraft Type of aircraft
National origin	Germany
Manufacturer	Gothaer Waggonfabrik
Number built	12

The Gotha Go 150 was a light aircraft designed at the German company Gothaer Waggonfabrik in the late 1930s. It was intended for civilian use, but ended up being used as a military trainer.

Development

In January 1937 Major Werner Junck, chief of the LC II, the technical wing of the Reichsluftfahrtministerium responsible for the development of new aircraft, informed various minor aircraft manufacturers such as Gothaer Waggonfabrik, Bücker, Fieseler, Flugzeugwerke Halle and Klemm that they would not get any contracts for the development of military aircraft. He therefore advised them to concentrate in the development of a Volksflugzeug or a small twin-engined plane. As a result, Gothaer Waggonfabrik developed the Go 150, while the other companies produced the Kl 105, the Si 202, the Bü 180 and the Fi 253.

The aircraft was a twin-engined monoplane with an enclosed cockpit. It was designed by Albert Kalkert, and first flew in 1937. The results of this flight were good, and production began. The aircraft was used to train both civilian and Luftwaffe pilots. The Go 150 was later also used in tests, where it was towed by a Heinkel He 46.^[1]

Specifications

Data from Flugzeug-Typenbuch : Handbuch der Deutschen Luftfahrt- und Zubehör-Industrie 1939/40^[2]

General characteristics

Crew: 1
Capacity: 1 pax
Length: 7.15 m (23 ft 5 in)
Wingspan: 11.8 m (38 ft 9 in)
Height: 2.03 m (6 ft 8 in)
Wing area: 17.5 m² (188 sq ft)
Aspect ratio: 7.88
Width folded: 3.85 m (13 ft)
Empty weight: 512 kg (1,129 lb)
Gross weight: 850 kg (1,874 lb)
Max takeoff weight: 1,036 kg (2,284 lb) ^{[citation needed]}
Fuel capacity: 150 L (40 US gal; 33 imp gal) fuel ; 7 L (1.8 US gal; 1.5 imp gal) oil
Powerplant: 2 × Zündapp Z 9-092 4-cylinder inverted air-cooled in-line piston engine 50 / 55 PS (49 / 54 hp; 37 / 40 kW) take-off/max continuous
Propellers: 2-bladed fixed-pitch wooden propellers, 1.55 m (5 ft 1 in) diameter
Propeller disc area: 3.76 m² (40.47 sq ft)
Propeller loading: 26.6 PS/m² (2.44 hp/sq ft; 19.6 kW/m²)

Performance

Maximum speed: 200 km/h (120 mph, 110 kn)
Cruise speed: 185 km/h (115 mph, 100 kn)
Landing speed: 70 km/h (43 mph; 38 kn)
Range: 750 km (470 mi, 400 nmi)
Endurance: 4 hours 5 minutes
Service ceiling: 4,500 m (14,800 ft)
g limits: +6.03 (ultimate)
Time to altitude: 1,000 m (3,300 ft) in 5 minutes 30 seconds
Wing loading: 48.5 kg/m² (9.9 lb/sq ft)
Power/mass: 0.118 PS/kg (0.053 hp/lb; 0.087 kW/kg)
Fuel consumption: 8.13 km/L (19.1 mpg_‑US; 23.0 mpg_‑imp)
Take-off run: 400 m (1,300 ft)
Landing run: 350 m (1,150 ft)

References

^ Kay. Antony L.; John Richard Smith; Eddie J. Creek (2002). German aircraft of the Second World War: including helicopters and missiles. Naval Institute Press. p. 276. ISBN 978-1-55750-010-6.
^ Schneider, Helmut (Dipl.Ing.) (1939). Flugzeug-Typenbuch : Handbuch der Deutschen Luftfahrt- und Zubehör-Industrie 1939/40 (Facsimile reprint 1988 ed.). leipzig: Gondrom. ISBN 3811206273.

Bibliography

Metzmacher, Andreas (2021). Gotha Aircraft 1913-1954: From the London Bomber to the Flying Wing Jet Fighter. Brimscombe, Stroud: Fonthill. ISBN 978-1-78155-706-8.

External links

Wikimedia Commons has media related to Gotha Go 150.

Luftarchiv - Fieseler Fi 253

Gotha aircraft

Company designations pre-1918

LD.1 LD.2 LD.3 LD.4 LD.5 LD.6 LD.7 LD.10
LE.1 LE.2 LE.3
WD.1 WD.2 WD.3 WD.4 WD.5 WD.7 WD.8 WD.9 WD.11 WD.12 WD.13 WD.14 WD.15 WD.17 WD.20 WD.22 WD.27

Idflieg designations 1914-1918

RLM designations 1933-1945

Project numbers

P.50
P.60

v t e Reich Air Ministry (RLM) aircraft designations (list)
1 to 100	8-1¹ Fi 2 8-3¹ 8-4¹ Fi 5 DFS 6 8-7¹ Gö 8 Gö 9 Do 10 Do 11/Wn 11 8-12⁴/Do 12 Do 13 Do 14 Do 15 Do 16/Wn 16 Do 17 Do 18 Do 19 Do 20 8-21¹ Do 22 Do 23 Do 24 Do 25³/Kl 25 Do 26/Kl 26 8-27/Do 27³/Kl 27⁵ 8-28¹ 8-29/Do 29 Fw 30 Kl 31 Kl 32 Ju 33 Ju 34 Kl 35 Kl 36 He 37³ He 38/Ju 38 DFS 39 BV 40/DFS 40 He 41³ Fw 42/He 42 Fw 43 Fw 44 He 45 He 46/Ju 46 Fw 47/He 47 Ju 48 He 49/Ju 49 He 50/Ju 50 He 51 He 52/Ju 52 Ju 53 DFS 54/NR 54 Fw 55/NR 55 Fw 56 8-57⁴/Fw 57 Fw 58/He 58 He 59 He 60/Ju 60 Fa 61/Fw 61/He 61 Fw 62/He 62 8-63⁴/He 63 Ar 64/He 64 Ar 65/He 65 Ar 66/He 66 Ar 67 Ar 68 Ar 69 He 70 8-71⁴/He 71 He 72 He 73³ He 74 Al 75 Ar 76/FZG 76⁶ Ar 77 Ar 78³ Ar 79 Ar 80 Ar 81 8-82⁴ 8-83¹ Al 84 Ju 85 Ju 86 Ju 87 Ju 88 Ju 89 Ju 90 Ju 91³ Ju 92 Ju 93³ Ju 94³ Ar 95 Ar 96 Fi 97 Fi 98 Fi 99 Fi 100³/He 100
101 to 200	Al 101 Al 102 Al 103/Fi 103 R Fh 104 Kl 105 Kl 106 Kl 107 Bf 108 Bf 109/Bf 109R⁶ Bf 110 He 111/He 111U⁶ He 112 He 113⁶ He 114 He 115 He 116 He 117³/Hs 117 He 118 He 119 He 120 Hs 121 Hs 122 Hs 123 Hs 124 Hs 125 Hs 126 Hs 127 Hs 128 Hs 129 Hs 130 Bü 131 Bü 132³/Hs 132 Bü 133 Bü 134 Ha 135 Ha 136/Hü 136 Ha 137 BV 138 Ha 139 Ha 140 BV 141 BV 142 BV 143 BV 144 Go 145 Go 146 Go 147/Ju 147 Go 148³ Go 149 Go 150 Kl 151 Kl 152/Ta 152 Kl 153³/Ta 153 Kl 154³/Ta 154 BV 155/Kl 155³/Me 155 Fi 156 Fi 157 Fi 158 Fw 159 Ju 160 Bf 161 Bf 162/He 162 Bf 163/Li 163/Me 163 Me 164/MeC 164 Bf 165 Fi 166/FK 166 Fi 167 Fi 168 Fi 169³ He 170 He 171³ He 172 He 173³ He 174³ 8-175⁴ He 176 He 177 He 178 He 179⁵ Bü 180/He 180 Bü 181 Bü 182 Bü 183³/Ta 183 Fl 184 Fl 185 Fw 186/Ju 186 Fw 187/Ju 187² Fw 188³/Ju 188 Fw 189 Fw 190 Fw 191 Ao 192 Ao 193³/DFS 193 DFS 194/Me 194 Ar 195 Ar 196 Ar 197 Ar 198 Ar 199/FiSk 199 Do 200^4,6/Fw 200
201 to 300	Si 201 Si 202 DFS 203 Si 204 8-205¹ Fw 206 8-207¹ Me 208 Me 209 (I)/Me 209 (II) Me 210 Hü 211 8-212⁴/Do 212 8-213¹ Do 214 Do 215 Do 216 Do 217/Hs 217 Do 218³ He 219 He 220 Do 221³ BV 222 Fa 223 Fa 224 Ao 225/Fa 225 BV 226/Ho 226 FGP 227 DFS 228 Go 229/Ho 229 8-230/DFS 230 Ar 231 Ar 232 Ar 233 Ar 234 Do 235⁵ Fa 236³ BV 237 BV 238 8-239¹ Ar 240 Go 241 Go 242 Me 243³ Go 244 Go 245³ BV 246 8-247¹ Ju 248 BV 250/Ho 250 Ho 251 Ho 252 Ju 252 Fi 253/Ho 253 Ho 254/Ta 254 8-255¹ Fi 256 SK 257 8-258¹ Fw 259 8-260¹ Me 261/Me 261w Me 262 Me 263 (1941)/Me 263 (1942)/Me 263 (1945) Me 264 Fl 265/Me 265 Fa 266/Go 266³ Ho 267 Ju 268 Fa 269 He 270 We 271 He 272³ He 273³ He 274 He 275⁵ He 276³ He 277 He 278 He 279³ He 280 He 281³ Fl 282 Fa 283 Fa 284 Fl 285 Ju 286 Ju 287 Do 288^4,6/Ju 288 Ju 289³ Ju 290 Hs 291 As 292/Hs 292³ Hs 293 Hs 294 Hs 295 Ar 296/Hs 296 Hs 297 Hs 298 Ju 299³ Fw 300
301 to 349	DFS 301 8-302¹ 8-303¹ 8-304¹ 8-305¹ 8-306¹ 8-307¹ 8-308¹ Me 309 Zwilling Me 310 8-311¹ 8-312¹ 8-313⁴ 8-314¹ Hs 315 8-316¹ Do 317 Do 318 He 319 Me 320³ Me 321 Ju 322 Me 323/ZMe 323 8-324¹ Fa 325/Fw 325³ 8-326¹ Me 327 Me 328 Me 329 Fa 330 DFS 331 DFS 332 Fi 333 Ar 334³/Me 334 Do 335 Fa 336 Ju 337³ 8-338¹ Fl 339 Ar 340 8-341 WNF 342 He 343 Rk 344/So 344⁵ Go 345 DFS 346 Rk 347 8-348¹ Ba 349
Post-349 (non-sequential)	Ju 352 Fi 356/Ju 356 Me 362 Me 364² Me 368³ Ju 388 Ju 390 Fw 391 Ar 393³ Ar 396 Ta 400 Me 409 Me 410 Do 417 He 419 ZMe 423 Ar 430/Ka 430 Ar 432 Do 435 Ar 440 8-445⁴ DFS 446 Ju 452 Me 462² DFS 468 Ju 488 Fw 491 He 500 Me 509 Me 510 He 519 8-520⁴ ZSO 523 Ar 532 8-534⁴ Do 535/He 535 Me 600² Me 609 Ar 632 Do 635/He 635/Ju 635
¹ Not assigned ² Unofficial/proposed ³ Assigned, but not used before RLM was dissolved ⁴ Assigned to captured aircraft ⁵ Unconfirmed ⁶ Propaganda/cover designation Note: Official RLM designations had the prefix "8-", but this was usually dropped and replaced with the manufacturer's prefix.

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