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Messerschmitt Me 263
Me 263 | |
---|---|
Type | Interceptor fighter |
Manufacturer | Messerschmitt/Junkers |
Designed by | Alexander Lippisch |
Maiden flight | August 1944 (Unpowered) |
Primary user | Luftwaffe |
Number built | 1 |
Developed from | Messerschmitt Me 163 |
The Messerschmitt Me 263 was a rocket-powered fighter aircraft developed from the Messerschmitt Me 163 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.
The Me 163B had two main shortcomings. One was a limited flight endurance, the second was the lack of a retractable landing gear. The latter meant that the aircraft had to land on a retractable skid. Both shortcomings prevented it from becoming an efficient fighter aircraft.
The Me 163C was an improved design with increased fuel tankage but still lacked retractable landing gear.
The project was then handed over to Heinrich Hertel of the Junkers company. This resulted in the aircraft becoming the Junkers Ju 248.
The design of the Ju 248/Me 263 started after the Me 163C because the Me 163C was not considered an adequate successor to the Me 163B because of its landing skid. The Ju 248/Me 263 took the wings and tail section of the Me 163B while the Me 263 was a completely new design.
Already on 25 September a wooden mock-up was shown to the officials. The fuselage was considerably modified to accommodate larger fuel tanks to give longer range, the cockpit was redesigned for pressurization and fitted with a bubble canopy to improve the rear view for the pilot, and the skid undercarriage was replaced with a conventional retractable undercarriage. The Walter rocket engine was modified to have two chambers - a main chamber to provide power for takeoff and climb, and an auxiliary chamber to provide lower power (and therefore lower fuel consumption) for cruising at altitude. The auxiliary chamber afforded a thrust of 300 kg (660 lb) which was in addition to the main chamber's normal thrust of 1,700 kg (3,750 lb), and the intention was that the aircraft should take off and climb to operational altitude with both rocket chambers operating at full thrust, then cut the main chamber and cruise on the power of the auxiliary chamber alone. This engine arrangement had previously been tested on modified Me 163Bs. The production version was intended to be powered by the more powerful BMW 708 rocket engine in place of the Walter powerplant.
Prior to the actual building of the Ju 248, two Me 163Bs were slated to be rebuilt, the V 13 and the V 18. Unfortunately, the V 13 was deteriorated due to weather attrition, so only the V 18 was rebuilt. It is this aircraft which is often identified as the Me 163D. However, it should be clear that there was no Me 163D as this aircraft was built AFTER the Ju 248 project had started. 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 and the Me 263 Scholle.
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. This meant two 160 litre (35 Imp gal, 42 US gal) external T-Stoff 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 early 1945 Junkers proposed its own project, the EF 127 Wally rocket fighter, as a competitor to the Me 163C and Me 263. This is typical for the German war industry where companies still tried to outbid each other instead of focusing resources on a common project.
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 at that time. The results of those first flights was that the aircraft gave a "ziemlich fertigen Eindruck", meaning 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 Führernotprogramm 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 continued.
At this point 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. They never flew under their own power but only as gliders. At this point they no longer exhibited the center of gravity problems.
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 USA. 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 lb)
Performance
- Maximum speed: 880 km/h (at 14,000 m)
- Service ceiling: 14,000 m (45,212 ft)
- Rate of climb: 750 m/sec ()
- Endurance:15 minutes at 11,000 m (36,090 ft)
(All performance figures estimated)Armament
- 2 x 30 mm MK 108 cannon in wing roots
External links
See also
Related development
Comparable aircraft
Designation sequence
Go 242 -
Go 244 -
BV 246 -
Ju 248 -
BV 250 -
Ho 250 -
Fw 250 -
Me 261 -
Fw 261 -
Me 262 -
Me 263 -
Me 264 -
Fl 265 -
Me 265
Related lists
List of military aircraft of Germany
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Records | Flight airspeed record · Flight distance record · Flight altitude record · Flight endurance record · Most produced aircraft |
Lists relating to aviation | |
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General | Timeline of aviation · Aircraft · Aircraft manufacturers · Aircraft engines · Aircraft engine manufacturers · Airports · Airlines |
Military | Air forces · Aircraft weapons · Missiles · Unmanned aerial vehicles (UAVs) · Experimental aircraft |
Notable incidents and accidents | Military aviation · Airliners · General aviation · Famous aviation-related deaths |
Records | Flight airspeed record · Flight distance record · Flight altitude record · Flight endurance record · Most produced aircraft |
Template:RLM aircraft designations
de:Junkers Ju 248 it:Messerschmitt Me 263 pl:Messerschmitt Me 263
This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Messerschmitt Me 263". |