Messerschmitt Me 263

Throughout development the RLM was disappointed 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 design of the 163C was followed to produce an even larger version, the Ju 248. It retained the new pressurized cockpit and bubble canopy of the 163C, with more fuel capacity, and added a new retractable landing gear. On September 25, 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.[1]

Prior to the assembly of the Ju 248, two Me 163Bs, v13 and v18, were slated to be rebuilt. V13 had deteriorated from weather exposure, so only v18 was rebuilt, but had been flown by test pilot Heini Dittmar to a record-setting 1,130 kilometres per hour (700 mph) 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 it 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 Sondergeräte (special equipment) in the form of a Zusatztreibstoffbehälter (auxiliary fuel tank): two 160 L (35 imp gal; 42 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.

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 shifted 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 first flights gave the impression that it was suitable as it was for production.

Test flights later had to be halted due to fuel shortages for the Bf 110 towplanes. Because the Me 263 was not 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 its armament built in. The next month both the v1 and the v2 had the dual-chamber 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 others were handed over to the Russians, who then created their own Mikoyan-Gurevich I-270 interceptor.