On July 15, 1944, the RLM submitted Proposal 226/II to Germany's aircraft manufacturers. This "Emergency Fighter Competition" specified the following requirements (although these were later to change several times) for the second-generation of jet-powered fighters for the Third Reich:
shape
on paper. The fuselage was short and wide, with two round air intakes on
either side of the cockpit, which fed the single He S 011 jet engine which
was located in the lower rear fuselage. 710 liters (188 gallons) of fuel
could be contained above and below the turbojet. The wings featured two
different sweepback angles, a steeper angle (40 degrees) near the fuselage
and a shallower angle (26 degrees) outboard. Flaps were located over the
entire trailing edge to aid in slow speed operations. Another 170 liters
(45 gallons) of fuel could be carried in wing tanks located in each of
the inner wing sections, making a total of 1050 liters (277 gallons). The
V-tail unit (110 degrees of separation) was mounted on a boom that extended
above the jet exhaust, a feature that would be present on all future Me
P.1101 designs. A steel plate was used on the underside of the tail boom,
to protect the enclosed radio equipment from engine exhaust heat. The nose
wheel of the tricycle landing gear retracted to the rear and the two main
wheels retracted forwards into the wing roots. A single SC 500 bomb could
be carried, partially stowed in a belly recess. The main armament was to
consist of two MK 108 30mm cannon, located in the lower forward fuselage
sides.
air
intakes, located on either side of the cockpit, fed the single He S 011
jet engine which was located in the rear fuselage. There were two protected
fuel tanks above the engine and behind the cockpit that held 830 kg (1830
lbs) of fuel. The wing was "borrowed" from the Me 262 outer wing, was swept
back at 40 degrees and mounted mid-fuselage. A V-tail was also to be fitted
on this design, with the jet engine exhausting below the tail boom. The
nose wheel retracted to the rear and rotated 90 degrees to lie flat beneath
the weapons bay in the nose. Both main wheels retracted inwards towards
the wing roots. Provisions were made for a drop tank, and even for a towed
fuel tank using the V-1 wing! The armament was to be either a MK 112 55mm
cannon or two MK 108 30mm cannons, with a possible third MK 108 or MK 103
30mm cannon being able to be squeezed in. One of the more advanced weapon
proposals for this design variant of the Me P.1101 was for the upward firing
SG 500 "Jagdfaust" (Fighter's Fist). This was basically a thin cased
50mm high explosive rocket propelled shell housed in a vertical tube. Two
of these would have been placed in the fuselage nose, and a single SC 500
bomb could also be carried beneath the fuselage.
accept
the Lorin ramjet tube, and the undercarriage was kept simplified and low
to the ground. Since a ramjet does not operate until a certain speed is
reached, eight solid-propellant rockets with 1000 kp thrust each would
be ignited to reach the ramjet's operating speed. Only a very short takeoff
distance would be needed, but the aircraft's range would be limited, thus
the Me P.1101L would have to be deployed near key Allied bombing targets.
beneath
the cockpit for the air duct. Located behind the cockpit and above the
engine was the fuel supply of 1000 liters (220 gallons). The rear fuselage
tapered down to a cone, where the radio equipment, oxygen equipment, directional
control and master compass were mounted. The underside of the rear fuselage
was covered over with sheet steel, for protection from the heat of the
jet exhaust. Although a Jumo 004B jet engine was planned for the first
prototype, the more powerful He S 011 could be added on later versions
with a minimum of fuss. The wing was basically the same as the Messerschmitt
Me 262 wing from the engine (rib 7) to the end cap (rib 21), including
the Me 262's aileron and leading edge slats. A second wing assembly was
delivered in February 1945, in which the leading edge slots had been enlarged
from 13% to 20% of the wing chord. The wing covered in plywood, and could
be adjusted on the ground at 35, 40 or 45 degrees of sweepback. Both the
vertical and horizontal tails were constructed of wood, and the rudder
could be deflected 20 degrees. Also under design was a T-tail unit and
a V-tail also. The undercarriage was of a tricycle arrangement. The nose
wheel retracted to the rear and was steerable. The main gear retracted
to the front, and included brakes. The cockpit was located in the nose,
with a bubble canopy giving good vision all around. The canopy was kept
clear by warm air which could be drawn from the engine. Cockpit pressurization
was to be incorporated in the production model, as was either two or four
MK 108 30mm cannon. The production model was also to fitted with cockpit
armor, and up to four underwing X-4 air-to-air missiles could be carried.
| Variant | Span | Length | Height | Wing Area | Track Width | Wing Sweep Angle |
| First Design
(July 24, 1944) |
7.15 m
23' 5" |
6.85 m
22' 9" |
2.45 m
8' |
2.1 m
6' 11" |
26 & 40 | |
| Second Design
(August 30, 1944) |
8.16 m
26' 9" |
9.37 m
30' 9" |
3.08 m
10' 1" |
13.5 m²
145.31 ft² |
40 | |
| Third Design
(Prototype) |
8.06 m
26' 5" |
8.98 m
29' 6" |
3.5 m
11' 6" |
13.6 m²
146.39 ft² |
2.124 m
6' 11" |
35/40/45 |
| Fourth Design
(Production) |
8.25 m
27' 1" |
9.175 m
30' 1" |
3.71 m
12' 2" |
15.85 m²
170.61 ft² |
2.2 m
7' 3" |
40 |
| Variant | Empty Weight | Takeoff Weight | Max. Wing Load | Fuel | |
| First Design
(July 24, 1944) |
3000 kg
6613.86 lbs |
800 kg
1763.69 lbs |
|||
| Second Design
(August 30, 1944) |
2642 kg
5824.61 lbs |
3554 kg
7835.22 lbs |
263 kg/m²
53.92 lbs/ft² |
830 kg
1829.84 lbs |
|
| Third Design
(Prototype) |
2184 kg
4814.89 lbs |
3205 kg
7065.81 lbs |
236 kg/m²
48.27 lbs/ft² |
830 kg
1829.84 lbs |
|
| Fourth Design
(Production) |
2594 kg
5718.78 lbs |
4064 kg
8959.57 lbs |
296.5 kg/m²
52.51 lbs/ft² |
1250 kg
2755.77 lbs |
| Variant | Max. Speed | Climb | Ceiling | Range | Landing Speed/Distance |
| First Design
(July 24, 1944) |
1050 km/h @ 6000 m
652 mph @ 19685' |
26.8 m/sec
88 ft/sec |
12000 m
39370' |
||
| Second Design
(August 30, 1944) |
1080 km/h @ 7000 m
671 mph @ 22966' |
30 m/sec
98 ft/sec |
14800 m
48556' |
1500 km
932 miles |
|
| Third Design
(Prototype) |
860 km/h @ 7000 m
534 mph @ 22966' |
12 m/sec
39 ft/sec |
10000 m
32808' |
170 km/h / 900 m
106 mph / 2953' |
|
| Fourth Design
(Production) |
985 km/h @ 7000 m
612 mph @ 22966' |
22.2 m/sec
73 ft/sec |
12000 m
39370' |
1500 km
932 miles |
172 km/h / 570 m
107 mph / 1870' |
| Manufacturer | Scale | Material | Notes |
| DML (Dragon) | 1/72 | Injected, photoetch & decals | includes He S 011 engine |
| DML (Dragon) | 1/72 | Injected, photoetch & decals | "Nachtjäger"version - includes photoetch
radar antenna & T-Tail |
| Huma | 1/72 | Injected & decals | includes different engines |
| Revell | 1/72 | Injected & decals | DML (Dragon) re-release without photoetched parts |
| MPM | 1/48 | Injected & decals | Not Yet Released |
| Ponkoz Model | 1/48 | Resin |
| 1) right wing, mounted 2) canopy wind shield 3) canopy center section 4) canopy discharge section 5) fuselage nose | |
| 6) center fuselage/ fuel
tanks 7) center fuselage 8) fuselage rear section 9) fuselage rear section 10) fuselage end cone 11) vertical tail 12) rudder 13) horizontal stabilizer 14) left elevator 15) right elevator 16) left landing flaps 17) left lateral control 18) left wing 19) outer leading edge slats 20) inner leading edge slats 21) lower engine cowling 22) left landing gear door 23) right landing gear door 24) right engine fairing 25) left engine fairing |
![]() |
| 26) landing gear nose wheel 27) right main landing gear 28) left main landing gear 29) He S 011 jet engine | |
Me P.1101 proposal dated October 3, 1944
| Me P.1101 drawing dated November 8, 1944 | ![]() |
Me P.1101 drawing from November 13, 1944

| The Messerschmitt Me P.1101 with T-Tail (top)
and V-Tail (bottom) ![]() |
The Me P.1101 instrument panel
The Me P.1101 wing assembly
|
A 1/10 scale
drawing of the proposed Me P.1101's horizontal tail unit ("T-Tail") dated
November 17, 1944 by Dr.Woldemar Voight
The Me P.1101 front landing gear arrangement drawing
The rear landing gear drawing for the Me P.1101
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On November 15, 1944, an experiment was performed using the Jumo 004
engine on a Me 262 to measure the loss of thrust due to a long intake.
The optimum shape was found to be a smooth, round intake, which resulted
in only a 3% loss of thrust.
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|
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| A good side view, showing the He S 011
mock-up engine installation ![]() |
Although a poorer quality photo, this shows off the typical side-hinging
Messerschmitt canopy
![]() |
A rear view of the Me P.1101
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Another rear view of the P.1101
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The damaged nose section of the P.1101
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|
| Bell Aircraft workers check out the Me P.1101.
Note the replaced damaged nose section. ![]() |
A nice front view of the Me P.1101
![]() |
| A side view of the P.1101 showing the placement of the
MG 151 mock-up cannon ![]() |
A close up showing the mock-up placement of
the MK 108 cannon on the P.1101 ![]() |
The Me P.1101 after the installation of a Allison J-35 jet engine
![]() |
A close-up of the Allison J-35 jet engine in the P.1101
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The Me P.1101 at Bell Aircraft Company in Buffalo, New
York
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|
The first Bell X-5 prototype (50-1838) still in Buffalo, N.Y.
![]() |
The Bell X-5 takes off for the first time from
Edwards AFB in California ![]() |
| An in-flight photo of the Bell X-5 second prototype (50-1839)
with the wings set for low speed ![]() |
The second X-5 prototype comes in for a landing
![]() |


Above images from: (top) Luftwaffe Secret Projects:
Fighters 1939-1945 - Midland Publishing
(center) Luftwaffe 1946 - Wydawnictwo Military
#12
(bottom) German Jets in WWII - Model Art Special
#348