Messerschmitt Me P.1101

infobox Aircraft
name =Me P.1101
type =Fighter
manufacturer =Messerschmitt


caption = The uncompleted P.1101 prototype
designer =Willy Messerschmitt
first flight =never flown
introduced =
retired =
status =
primary user = Luftwaffe (intended)
more users =
produced =
number built = 1
unit cost =
developed from=
variants with their own articles =

Messerschmitt P.1101 was the name attached to a single-seat, single-jet fighter developed in response to the July 1944 Emergency Fighter Program, which sought the second generation of jet fighters for the Third Reich. A characteristic feature of the Me P.1101 prototype was that the sweep of the wings could be changed before flight, a feature perfected by the later Variable-sweep aircraft such as the Bell X-5, the General Dynamics F-111, and the F-14 Tomcat.

Design and development

Within nine days of the 15 July 1944 issuance of the design specifications for the Emergency Fighter, the Messerschmitt design bureau had formed a preliminary paper design for the P.1101. The aircraft which was developed initially had a short and wide fuselage, tricycle landing gear, and mid-mounted wings with an inner sweep of 40 degrees near the fuselage, and a shallower 26 degree angle outboard. The single He S 011 jet engine was to be mounted internally within the fuselage, being aspirated by two rounded intakes located on either side of the cockpit. The tail was of a V configuration, and mounted on a tapered boom which extended over and past the jet exhaust, while the cockpit was forward mounted, with the canopy integrated into the fuselage and forming part of the rounded nose of the aircraft.

By late August 1944, the still paper design had evolved into a sleeker incarnation, with the previously stout fuselage lengthened and narrowed, and a conical nose section was added in front of the cockpit. The double angled wing was also abandoned, with the outer wing of the Me 262 instead being adapted for the design. The design was further developed, and after the wind tunnel testing of a number of wing and fuselage profiles, the design was further modified and finalized, with the decision made to undertake the construction of a full-scale test aircraft. This finalized design and associated test data were submitted to the Construction Bureau on 10 November 1944 and the selection of production materials was begun on 4 December 1944.

Production prototype

The worsening war situation led to the expedited, but risky approach of building a full-scale prototype in parallel with detail construction and continuing statistical calculation, while existing components such as the wings, landing gear, and flight components were utilized where feasible. It was also intended for the test flights to be conducted with both 35 and 45 degree wing sweep. Production of the V1 prototype was begun at Messerschmitt's Bavarian Oberammergau Complex with a projected first flight in June 1945.

The Me P.1101 V1 prototype was of duralumin fuselage construction, retained the outer wing section of the Me-262 and as mentioned previously, the wing sweep could be adjusted on the ground from 30, 40, to 45 degrees, making it a forerunner of later variable-geometry designs. The tandem, fuselage mounted intakes of the preliminary designs were replaced by a single nose intake, and the canopy became a bubble design, which afforded better all-around vision than the initial integrated canopy offered. The production prototype also incorporated a more conventional T-tail design, which was constructed out of wood and remained mounted on the tapered tail boom. The tricycle undercarriage consisted of a steerable, rear retracting nose wheel and wing root mounted main gear, which was forward retracting. The prototype was fitted with a Jumo 004B jet engine, which could easily be replaced with the more powerful He S 011 in subsequent full production versions. In addition, the production model was to be equipped with a pressurized cockpit and armored canopy.

Postwar

By the time an American infantry unit discovered the Oberammergau complex on 29 April 1945 the V1 prototype was approximately 80% complete. The airframe was removed from the nearby tunnel in which it was hidden and all associated documents were seized. There was some lobbying by Messerschmitt Chief Designer Woldemar Voight and Robert J. Woods of Bell Aircraft to have the Me P.1101 V1 completed by June 1945, but this was precluded by the destruction of some critical documents and the refusal of the French to release the remaining majority of the design documents, which they had obtained prior to the arrival of American units to the area. Fact|date=December 2007

The prototype was finally shipped to the Bell Aircraft Works in Buffalo, New York in 1948, and the already damaged aircraft suffered further damage when it fell off a freight car. This damage ruled out any possibility for repair although the Me P.1101 design components were subsequently used by Bell as the basis for the Bell X-5, which was the first aircraft capable of varying its wing geometry while in flight. The remnants of the P.1101 were scrapped in the early 1950s.

pecifications (Me P.1101 V1 Prototype)

aircraft specifications
plane or copter?=plane
jet or prop?=jet
ref=
crew=one, pilot
capacity=
payload main=
payload alt=
length main= 8.98 m
length alt= 29 ft 5 in
span main= 8.06 m
span alt= 26 ft 5 in
height main= 3.5 m
height alt= 11 ft 6 in
area main= 13.6 m²
area alt= 146 ft²
airfoil=
empty weight main= 2,594 kg
empty weight alt= 5,718.78 lb
loaded weight main= 4,064 kg
loaded weight alt= 8,960 lb
useful load main=
useful load alt=
max takeoff weight main= 4,500 kg
max takeoff weight alt= 9,900 lb
more general=
* Fuel capacity : 1,000 liters (264 gallons)
engine (jet)=Jumo 004B
type of jet=
number of jets=1
thrust main=
thrust alt=
thrust original=
afterburning thrust main=
afterburning thrust alt=
max speed main= 980 km/h (Mach 0.8)
max speed alt= 612.5 mph
cruise speed main= 985 km/h at 7,000 m
cruise speed alt=616 mph at 22,965 feet
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main= 1,500 km
range alt=932 miles
ceiling main= 12,000 m
ceiling alt= 39,370 ft
climb rate main= 22.2 m/s
climb rate alt= 73 ft/s
loading main=236 kg/m²
loading alt=42.87 lb/ft²
thrust/weight=
power/mass main=
power/mass alt=
more performance=
* Max wing loading : 296.5 kg/m²
armament=
* None for prototype
* 2 or 4 × 30 mm MK 108 cannons and 4 × X-4 air-to-air missiles on production version
avionics=

ee also

aircontent
related=
*Messerschmitt Me P.1106

similar aircraft=
* Bell X-5
* Short SB5
* Saab Tunnan

sequence=

lists=
* List of World War II military aircraft of Germany

see also=

References

* Winchester, Jim. "Bell X-5." "Concept Aircraft: Prototypes, X-Planes and Experimental Aircraft". Kent, UK: Grange Books plc., 2005. ISBN 1-84013-309-2.

External links

* [http://www.luft46.com/mess/mep1101.html Luft '46 entry on the Me P.1101]
* [http://www.airbornegrafix.com/HistoricAircraft/MeP1101.htm Airbornegrafix page]
* [http://hsfeatures.com/me1101_pk.htm Build a scale model of the p.1101]