Messerschmitt Me 263

For the fictional aircraft of this designation from Aces: Iron Eagle III, see Messerschmitt Me 263 (fictional).

Me 263

Model of Me 263
Role	Fighter-Interceptor
Manufacturer	Messerschmitt/Junkers
Designer	Alexander Lippisch
First flight	August 1944 (Unpowered)
Primary user	Luftwaffe
Number built	1
Developed from	Messerschmitt Me 163

The Messerschmitt Me 263 Scholle (plaice)^[1] was a rocket-powered fighter aircraft developed from the Me 163 Komet towards the end of World War II. Three prototypes were built but never flown under their own power as the rapidly deteriorating military situation in Germany prevented the completion of the test program.

History

Although the Me 163 had very short endurance, it had originally been even shorter. In the original design, the engine had only one throttle setting, "full on", and burned through its fuel in a few minutes. Not only did this further limit endurance, in flight testing, pilots found the aircraft quickly exhibited compressibility effects as soon as they levelled off from the climb and speeds picked up. This led the RLM to demand the addition of a throttle, leading to lengthy delays and a dramatic decrease in fuel economy when throttled.

This problem was addressed in the slightly updated Me 163C. This featured the same HWK 509B or -C dual chamber rocket engine already trialled on the Me 163B V6 and V18 prototypes; the main upper chamber was tuned for high thrust while the lower Marschofen combustion chamber was designed for a much lower thrust output (about 400 kgf maximum) for economic cruise. In operation, throttling was accomplished by starting or stopping the main engine, which was about four times as powerful as the smaller one. This change greatly simplified the engine, while also retaining much higher efficiency during cruise. Along with slightly increased fuel tankage, the powered endurance rose to about 12 minutes, a 50% improvement. As the aircraft spent only a short time climbing, this meant the time at combat altitude would be more than doubled.

Ju 248

Throughout development the RLM proved unhappy with the progress on the 163 project, and eventually decided to transfer development to Heinrich Hertel at Junkers. Lippisch remained at Messerschmitt and retained the support of Waldemar Voigt, continuing development of the 163C.

At Junkers, the basic plan of the 163C was followed to produce an even larger design, the Ju 248. It retained the new pressurized cockpit and bubble canopy of the 163C, with even more fuel tankage and a new retractable landing gear design. On 25 September 1944 a wooden mock-up was shown to officials. The production version was intended to be powered by the more powerful BMW 109-708 rocket engine in place of the Walter power plant. It was also intended to have retractable landing gear.^[2]

Prior to the actual building of the Ju 248, two Me 163Bs, V13 and V18, were slated to be rebuilt. V13 had deteriorated due to weather exposure, so only V18 was rebuilt, but had been flown by test pilot Heini Dittmar at a record-setting 1,130 km/h (702 mph) velocity on July 6, 1944 and suffered near-total destruction of its rudder surface as a result.^[3]^[4]^[5] It is this aircraft that is often identified as the Me 163D, but this aircraft was built after the Ju 248 project had started.

Hertel had hoped to install Lorin ramjet engines, but this technology was still far ahead of its time. As a stopgap measure, they decided to build the aircraft with a Sondergerät (special equipment) in the form of a Zusatztreibstoffbehälter (auxiliary fuel tank): two 160 l (35 imp gal) (42.2 US gal) external T-Stoff oxidizer tanks were to be installed under the wings. This would lead to a 10% speed decrease but no negative flight characteristics. Although Junkers claimed the Ju 248 used a standard Me 163B wing, they decided to modify the wing to hold more C-Stoff fuel. This modification was carried out by the Puklitsch firm.

Me 263

In November 1944, the aircraft was again redesignated as the Me 263 to show its connection with the Me 163. The two projects also got names - the Ju 248 Flunder (Flounder) and the Me 263 Scholle (Plaice). In early 1945, Junkers proposed its own project, the EF 127 Walli rocket fighter, as a competitor to the Me 163C and Me 263.

The first unpowered flight of the Me 263 V1 was in February 1945. Several more unpowered flights took place that month. The biggest problem had to do with the center of gravity which was restored with the addition of counterweights. Eventually, the production aircraft would have repositioned the engine or the landing gear installation to solve this problem. The landing gear was still non-retractable. The results of those first flights was the aircraft gave a "ziemlich fertigen Eindruck", meaning that it seemed to be ready.

Test flights were later stopped because of fuel shortages for the Bf 110 towplanes. As the Me 263 was not a part of the Jägernotprogramm (Emergency Fighter Program), it was difficult to get the resources it needed. For the time being the plane was not expected to enter production but further development was allowed. The V2 and V3 were not yet ready. The V2 was to get the retractable landing gear and the V3 would have the armament built in. The next month both the V1 and the V2 had the two-chambered HWK 109-509C installed, correcting the center-of-gravity problems. They flew only as gliders.

In April, the Americans occupied the plant and captured the three prototypes and the mock-up. The V2 was destroyed but another prototype ended up in the US. The rest was handed over to the Russians, who then created their own Mikoyan-Gurevich I-270 interceptor.

Specifications (Me 263 V1)

General characteristics

Crew: 1
Length: 7.83 m (25 ft)
Wingspan: 9.50 m (31 ft 2 in)
Height: 3.17 m ()
Wing area: 17.80 m² (191.59 ft²)
Empty weight: 2,105 kg (4,640 lb)
Max. takeoff weight: 5,150 kg (11,354 lb)
Powerplant: 1 × Walter HWK 109-509C-3 rocket, 19.61 kN (4,410 lbf)

Performance

Maximum speed: 880 km/h (550 mph) (14,000 m (45,000 ft))
Service ceiling: 14,000 m (45,212 ft)
Rate of climb: 150 m/s (29,500 fpm)
Endurance:15 minutes at 11,000 m (36,090 ft)
(All performance figures estimated)

Armament

2 × 30 mm (1.18 in) MK 108 cannons in wing roots

Notes

↑ Christopher, John. The Race for Hitler's X-Planes (The Mill, Gloucestershire: History Press, 2013), p.142.
↑ Christopher, p.142.
↑ Käsemann 1999, pp. 17, 122.
↑ de Bie, Rob. "Me 163B Komet - Me 163 Production - Me 163B: Werknummern list." robdebie.home. Retrieved: 28 July 2013.
↑ "Me 163." walterwerke.co.uk. Retrieved: 28 August 2010.

References

Wikimedia Commons has media related to Messerschmitt Me 263.

David Myhra, "Messerschmitt Me 263", Schiffer Publishing, 1999. ISBN 0-76430-909-9.
Christopher, John. The Race for Hitler's X-Planes. The Mill, Gloucestershire: History Press, 2013.

Messerschmitt aircraft

Company designations	M 17 M 18 M 19 M 20 M 21 M 22 M 23 M 24 M 25 M 26 M 27 M 28 M 29 M 30 M 31 M 33 M 35 M 36 M 37

RLM designations 1933–45	Bf 108 Bf 109 Bf 109TL Bf 110 Me 155 Bf 161 Bf 162 Bf 163 Me 163 Bf 165 Me 209 Me 210 Me 261 Me 262 Me 263 Me 264 Me 265 Me 309 Me 310 Me 321 Me 323 Me 328 Me 329 Me 334 Me 409 Me 410 Me 509 Me 609

Experimental designations	P 08.01 P.1070 P.1073 P.1075 P.1079 P.1092 P.1095 P.1099 P.1100 P.1101 P.1102 P.1103 P.1104 P.1106 P.1107 P.1108 P.1109 P.1110 P.1111 P.1112

USAAC designations	C-44

Junkers aircraft designations by designating body

Company	J 1 J 2 J 3 J 4 J 5 J 6 J 7 J 8 J 9 J 10 J 11 J 12 F 13 J 15 K 16 K 17 J 18 T 19 A 20 H 21 / J 21 / T 21 J 22 T 23 G 23 F 24 / G 24 A 25 T 26 T 27 J 28 T 29 K 30 G 31 A 32 W 33 W 34 A 35 S 36 K 37 G 38 K 39 K 47 A 48 A 50 K 51 K 53

Idflieg	CL.I D.I E.I J.I

RLM	Ju 46 Ju 49 Ju 52 Ju 60 Ju 85 Ju 86 Ju 87 Ju 88 Ju 89 Ju 90 Ju 160 Ju 187 Ju 188 Ju 248 Ju 252 Ju 268 Ju 287 Ju 288 Ju 290 Ju 322 Ju 352 Ju 388 Ju 390 Ju 488 Ju 635

"EF" (experimental)	EF 61 EF 126 EF 127 EF 128 EF 131 EF 132 EF 140 EF 150

Reich Air Ministry aircraft designations

1 to 100	B 9 Gö 9 Do 10 Do 11 Wn 11 Do 12 Do 13 Do 14 Do 15 Wn 15 Do 16 Wn 16 Do 17 Do 18 Do 19 Do 20 Do 22 Do 23 Do 24 Kl 25 Do 26 Kl 26 M 27 Do 29 Kl 31 Kl 32 W 33 L 33 W 34 Kl 35 Kl 36 HD 37 HD 38 G 38 DFS 39 BV 40 DFS 40 A 40 Fw 42 He 42 Fw 43 HD 43 Fw 44 He 45 He 46 Ju 46 Fw 47 Ju 47 K 47 A 48 He 49 Ju 49 He 50 A 50 He 51 K 51 Ju 52 K 53 NR 54 Fw 55 NR 55 Fw 56 Fw 57 Fw 58 He 58 He 59 He 60 Ju 60 Fw 61 He 61 Fw 62 He 62 He 63 Ar 64 He 64 Ar 65 He 65 Ar 66 He 66 Ar 67 Ar 68 Ar 69 He 70 He 71 He 72 He 74 Ar 76 Ar 77 Ar 79 Ar 80 Ar 81 Ju 85 Ju 86 Ju 87 Ju 88 Ju 89 Ju 90 Ar 95 Ar 96 Fi 97 Fi 98 Fi 99 He 100

101 to 200	Al 101 Al 102 Al 103 Fi 103 Fh 104 Kl 105 Kl 106 Kl 107 Bf 108 Bf 109 Bf 110 He 111 He 112 He 113 He 114 He 115 He 116 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 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 149 Go 150 Kl 151 Ta 152 Kl 152 Ta 153 Ta 154 BV 155 Fi 156 Fi 157 Fi 158 Fw 159 Ju 160 Bf 161 He 162 Bf 162 Bf 163 Me 163 Me 164 Fi 166 FK 166 Fi 167 Fi 168 He 170 He 172 He 176 He 177 He 178 Bü 180 Bü 181 Bü 182 Ta 183 Fl 184 Fl 185 Fw 186 Ju 186 Fw 187 Ju 187 Ju 188 Fw 189 Fw 190 Fw 191 Ao 192 DFS 193 DFS 194 Ar 195 Ar 196 Ar 197 Ar 198 Ar 199 Fw 200

201 to 300	Si 201 Si 202 DFS 203 Si 204 Fw 206 Me 208 Me 209 Me 209 (1943) Me 210 Hü 211 Do 212 Do 214 Do 215 Do 216 Do 217 Hs 217 He 219 He 220 BV 222 Fa 223 Fa 224 Ao 225 Fa 225 BV 226 Ho 226 FGP 227 DFS 228 Ho 229 DFS 230 Ar 231 Ar 232 Ar 233 Ar 234 Do 235 BV 237 BV 238 Fw 238 Ar 239 Ar 240 Go 241 Go 242 Go 244 BV 246 Ju 248 BV 250 Fw 250 Ho 250 Ho 251 Ho 252 Ju 252 Fi 253 Ho 253 Ta 254 Ho 254 Fi 256 Sk 257 Fw 261 Me 261 Me 262 Me 263 Me 264 Fl 265 Me 265 Fa 266 Ho 267 Ju 268 Fa 269 He 270 We 271 Fw 272 He 274 He 275 He 277 He 278 He 280 Fl 282 Fa 283 Ta 283 Fa 284 Fl 285 Ju 286 Ju 287 Ju 288 Ju 290 Me 290 As 292 Hs 293 Hs 294 Hs 295 Ar 296 Hs 296 Hs 297 Hs 298 Fw 300

301-	Me 309 Me 310 Do 317 Do 318 He 319 Me 321 Ju 322 Me 323 Me 328 Me 329 Fa 330 DFS 331 DFS 332 Fi 333 Me 334 Do 335 Fa 336 Fl 339 E.340 WNF 342 He 343 Rk 344 So 344 Go 345 DFS 346 Rk 347 Ba 349 Ju 352 Me 362 Me 364 Ju 388 Ju 390 Fw 391 Ar 396 Ta 400 Me 409 Me 410 Do 417 He 419 ZMe 423 Ar 430 Ka 430 Ar 432 Do 435 Ar 440 Ju 452 Me 462 Ju 488 Fw 491 Me 509 Me 510 He 519 ZSO 523 Ar 532 Do 535 E.555 Me 609 Ar 632 Do 635

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