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![]() Before the end of the WW II about half a dozen gruppen used Me 262 fighters. Also some radar-equipped Me 262B-1a/U1 nightfighters were used in last weeks of war. Bober versions of Me 262 also entered service alongside with reconnaisse planes. The apperance of German jets caused some consern to the Allies on account of their high speed and heavy armament.
18.03.2004 New feedbackform |
High-speed fighter | Interceptor fighter | Power plant | One turbojet | One turbojet | Crew | One | One | Installation of weapons | Possibly in the fuselage, or close to the fuselage | Armament | 2x MG 17 machine-guns with 1000 rpg, 1x MG 151/20 cannon with 500 rounds | 2x MG 17 machine-guns with 1000 rpg, 1x MG 151/20 cannon with 250 rounds | Installation of weapons | Possibly in the fuselage, or close to the fuselage | Possibly in the fuselage, or close to the fuselage | Radio | FuG VII | FuG VII | Maximum speed | 900 km/h | 900 km/h | Filght duration | 1h at maximum performance | 30mins at maximum performance | Airframe | Complete metal construction throughout. Simple and cheapiest construction is required. | Complete metal construction throughout. Simple and cheapiest construction is required. |
The first concrete proposal for the fighter evolved from series of quite different design studies: Becouse of RLM requirements for one turbojet, team began to consider signle engine layout. The first proposal was to mount the engine inside the fuselage with an intake extreme nose (like F-86 and Mig-15). This was quickly abandoned in favor of a twin-boom arangement (like Vampire). Third version was a pod and boom layout, witch redused the fuselage cross section and total wetted areas to minumum. This was abandoned, only to be empoyed five years later in P 1101 (Americans built Bell X-5 based on this), becouse single engine could not offer enough performance.
After twin-engine configuration had been selected, the first configuration was a straightforward low-wing plane with engine nacelles mounted centrally in the wings. The main undercacarriage units were located to retracted into wing fuselage intersection, one before other. This was not possible however to make this configuration, even if it would have offered optimum drag.
The Messershmitt AG began with concept designated Project (P) 1065, following these studies, in 1 April 1939. This proposal had virtually same wing as early Bf 109 and it was to be powered two BMW TL turbojet.
There were also suggested larger 22m2 wing and three different armament combinations by September 1939.
The first drawing of the P 1065 is from 17 October 1939 and it has oval fuselage, mid wing ans tricycle undercarriage. For the next several months, a steady stream of refinements would be made including, fuselage shape and cross section, wing location and shape, engine placement and landing gear configuration. Study triangular fuselage and low-mounted wing was preferred by many reasons including main undercarriage problem.
Two engine layouts were proposed: two BMW P.3302 engines under the wings or two slimmer BMW P.3304 engines mounted centrally. The Junkers T 1 (Jumo 004 A) engines entered picture in November 1939.
After presentation of cockpit and aircraft mockups in December 1939 and January 1940, the RLM ordered twenty prototype aircraft. Under this provisional contract, tooling and jigging work for two prototypes, began in January 1940. The first prototype layout was described by February 1940. The plane had two BMW P.3302 engines under the wings and leading edge of the outer wing sections were swept back 18 degrees. This was becouse BMW engineers reported production versions of their P.3302 prototype would be larger in diameter and heavier than originally anticipated. Also Junkers T 1 engines were being consired as alternative. Various placement options for the engines, forexample overwing, were examined via wind tunnel testing in June 1940. These refinements plus others, forexample redesigned fuselage and its cross-section (now embracing the familiar triangular shape), gave rise to P.1065/III officially submitted to the RLM in October 1940. Armament was standardized to three MG 151 cannons. Also other was suggested like ejection seat, braking parashute, pressurized cabin and dive breaks were proposed but never entered final product.
In order to get the prototype flying as soon as possible a single piston engine (Jumo 210 G)was to be fitted in the nose. On 10 January Messerchmitt proposed that first prototype would be powered with two rocket engines and piston engine in the nose. But also rocet motors ran into development problems an the idea was soon dropped. Construction of the first P 1065 prototype took place between February and March 1941. Project recieved the official RLM designation Me 262 on 8 April 1941.
Construction of the first prototype Me 262V1 began in January 1941. The first flight tests would take place without
engine nacelles, and with Jumo 210Ga 12-sylinder engine with two blade propeller. The later flights would include
nacelles to evaluate their effects on aerodynamics. Practical testing began as of 17 April 1941 with taxiing tests.
On 18 April Me 262V1 had its first flight which lasted 18 minutes. The flight caracteristics were discovered
satisfactory. Prototype could attain maximum speed of 420 km/h in level flight and 540 km/h in a dive. The RLM was
becoming more interested in the aircraft, ordering five more V-series and twenty 0-series Me 262 in 25 July 1941.
By the summer of 1942, five prototypes with BMW 003 turbines had been planned.
Although both jet engines Jumo and BMW shoved more promise, Messerschmitt still consired alternative engines for
second prototype. This time alternative engines were Argus impulse duct engines. These engines were simple but
extreamly fuel-consuming. This idea was abandond when engines progressed to flight tests, becouse it was found that
vibrations inducted by its intermittent operation made it dangerous to use the engine to normal service aircraft.
The Argus pulsejet was later used in V-1 flying bomb.
23 flights was done with only Jumo 210Ga engine. In February 1942 pair of BMW P.3302 pre-production engines were
fitted into nacelles and number of ground tests were conducted. The first fligt of the Me 262 under jet power took
place on 25 March 1942. There was still Jumo piston engine alongside with BMW jet engines.
Just after takeoff, about altitude of 10 m when jet engines one after one flamed out. This forced testpilot Fritz
Wendel to land heavily laden aircraft only with a piston engine. The jet engines were immeditely removed and cheked
and it was found that the compressor blades were broken in both engines. It was determined that the BMW 003 engine
needed to be totally redesigned.
Fortetunately in the meantime Jumo had succeeded overcoming most of the problems of their engine. The Me 262 design
was modified to accommodate larger and heavier Jumo 004 engines. On 1 June 1942 the first two engines were delivered
to Messerschmitt. The second and third prototypes (V2 and V3) were the first ones to accommodate the Jumo engines.
Me 262 Prototypes
Model | Variant | Description | A-1a | 4 MK 108 guns. Most common version | U1 | Two 20mm MG 151 cannon with 146 rounds each, two 30mm MK 103 cannon with 72 rounds each, and two 30mm MK 108 cannon with 66 rounds each. The MK 103 had a longer barrel and a higher muzzle velocity than the MK 108. Produced only test versions | U2 | One seat night finghter with radar. Only one produced | U3 | Recocnaisse with one MK 108 gun or without guns | U4 | 50mm cannon in the nose. This was intended to be the ultimate bomber-killer. | U5 | Fighter with six MK 108 cannon, two with 100 rounds, two with 85 rounds and two with 65 rounds. Only one produced | A-1b | The BMW 003 turbojet engines instead of the Jumo 004 turbojets used in the A-1a | A-2a | Fighter-bomber or "Jabo" | U1 | Fighter-bomber with TSA. Three prototypes | U2 | Lofte cabin (two crew mebers) Fighter-bomber | B-1a | Two seat treiner | U1 | Two seater night fighter | C-1a | Jumo 004 turbojets and rocet motor in the tail | C-2b | BMW 003 turbojets and two rocet motors above engines |
Versuchs number | Werk.Num. | Registration | Testing Assingments | Model | V1 | 262 000001 | PC+UA | Aerodynamic tests, engine tests (BMW) | V2 | 262 000002 | PC+UB | Performance and calibration tests | V3 | 262 000003 | PC+UC | Engine tests (Jumo) | V4 | 262 000004 | PC+UD | Engine tests (Jumo) | V5 | 262 000005 | PC+UE | Nose landing gear tests, take-off aid | + | two 20mm MG 151 cannon + two 30mm MK 103 cannon + two 30mm MK 108 cannon test | A-1a/U1 | V484 | 110484 | + | Lofte cabin, course control | A-2a/U2 | V11/V555 | 110555 | + | Lofte cabin II, navigation | A-2a/U2 | 111355 | + | Weapon system with 6 MK 108 | A-1a/U5 | 111358 | + | High speed fighter | HG II | 111857 | + | Inproved production model | - | 111899 | + | weapon system with MK 214 | A-1a/U4 | 111994 | + | Rocet launcher 21, R100 | A-1a | 112355 | + | Weapon system with six MK 108 | A-1a/U5 | V6 | 130001 | VI+AA | Engine tests (Jumo), hydraulically fully-retactable landing gear | A-0 | V7 | 130002 | VI+AB | Pressurized cabin | A-0 | V8 | 130003 | VI+AC | Revi 16b gunsight tests | A-0 | V9 | 130004 | VI+AD | Towed-bomb tests | A-0 | V10 | 130005 | VI+AE | Wooden drop tanks, towed-bomb tests | A-1a | 130010 | + | two-seat version | B-1a | 130018 | E3+01 | Engine tests (Jumo) | A-1a | 130170? | + | Engine tests (BMW) | A-1b | 130163 | E2+01 | Landing gear tests | A-1a | 130164 | WA+TA | Weapons & TSA tests | A-1a/U1 | 130165 | E4+E5 | Hydraulic & FT tests | A-1a | V5/V167 | 130167 | SQ+WF | Jettisonable tanks, brakes | A-1a | 130168 | E3+02 | High-altitude engine tests | A-1a | 130170 | E2+02 | Performance tests | A-1a | 130172 | EK+L1 | Fuel & tire tests | A-1a | 130174 | EK+L2 | Long-term tests | A-1a | 130175 | + | General flight tests | A-1a | V9/V186 | 130186 | + | Homeland Defender I | C-1a | 130188 | E7+01 | Diving sight, BZA, TSA | A-1a/U1 | 130189 | + | Flight tests | A-1a | 170038 | E3+03 | Engine tests (Junkers) | A-1a | 170039 | E3+L3 | Long-term engine tests | A-1a | V2/V56 | 170056 | + | Take-off aid, stability tests, FuG 218, 266 | A-1a/U2 | 170057 | WA+02 | Weapon tests | A-1a | 170070 | E7+02 | TSA, drop tests | A-1a | V074 | 170074 | + | Homeland Defender II | C-2b | V078 | 170078 | + | Engine tests (BMW 003 A-1) | A-1b | 170079 | + | Wheel drive tests | A-1a | V083 | 170083 | + | MK 214, taxiing tests | A-1a/U4 | 170086 | + | Stability, jettisonable tanks | A-1a | 170095 | + | Landing gear, night tests | A-1a | V7/V303 | 170303 | + | Drop tests to 1000 kg | A-1a | 170394 | + | General flight tests | A-1a | 500095 | + | Two Rb 50/30 cameras | A-4a |
Links:
Tamiya Me-262 model
References:
Warbird Tech Series vol 6: Messerschmitt Me 262 Sturmvogel (ISBN: 0-933424-69-8)
Feedback
Classic Publications
Stormbird: Flying through fire as a Luftwaffe
ground- attack pilot and Me 262 ace, book review
Me-262A-2a, Black X
The Messerschmitt Me-262 Schwalbe / Sturmvogel
Shiffer Military History VOL 23: The World´s First Turbojet Fighter Me 262 (ISBN: 0-88740-234-8)
Shiffer Military History VOL 64: Messerchmitt Me 262 (ISBN: 0-88740-410-3)
Classic Books: Me-262 vol 1 (ISBN: 0-903223-10-5)
Classic Books: Me-262 vol 2 (ISBN: 0-9526867-23)
Classic Books: Me-262 vol 3 (ISBN: 1-903223-00-8)
http://www.stormbirds.com/