In the summer
of 1943, Messerschmitt built on an earlier design, the Messerschmitt
Me P.1092A, with a further series of small, single-seat, single-jet
fighters. Hans Hornung led the design team, along with Woldemar Voigt and
Willie Messerschmitt himself. The first design, the Me P.1092/1, was very
similar to the Messerschmitt Me P.1092A, except
a normal fin/rudder and horizontal tail planes were fitted to the rear,
a variable sweep wing was added and the nosewheel was located aft of the
air intake.
With the Me P.1092/2, Messerschmitt changed the overall look of the P.1092.
The fuselage was short and squat, and the cockpit was faired into the rear
fuselage where the tail section began. The wings (mounted mid-fuselage,
with slight dihedral) were swept back at 21.5 degrees, and a provision
was made in the design for an extended wing. Again, the outer wing sections
of the Me 262 were used (for the extended wing version). Fuel capacity
was increased to 1250 liters (274 gallons), which was achieved by rearranging
the internal components. A more conventional tail unit was designed, and
was mounted on a boom under which the single Jumo 004C (1015 kg, 2237 lbs
thrust) exhausted. Also, the tail unit, with it's single fin and rudder
and high mounted tail planes, resembled the Messerschmitt Me 262 tail.
The landing gear arrangement was of a tricycle type, with the main gear
retracting inwards, and the forward gear retracted to the rear. Armament
was fairly heavy for a small fighter; it consisted of two MK 103 30mm cannon
(the length of the MK 103 necessitated that the barrels protruded from
the fuselage) and two MG 151/15 15mm cannon. All guns were mounted in the
forward fuselage on either side of the air intake.
The Me P.1092/2
was used in a performance comparison with the Lippisch
Me P.20. The P.1092/2 was judged superior in almost all categories.
Although the Me P.1092/2 was not constructed, it was used to gain experience
and design knowledge, especially with the later Me
P.1106 and Me P.1101 designs.
Span | Length | Height | Wing Area | Aspect Ratio | |
Normal
Wing |
7.75 m
25' 5" |
8.1 m
26' 6" |
3.65 m
11' 10" |
12.7 m²
136 ft² |
4.73:1 |
Extended
Wing |
10.0 m
32' 9" |
8.1 m
26' 6" |
3.65 m
11' 10" |
14.45 m²
155 ft² |
6.92:1 |
Empty Equipped Weight | Loaded Weight* | Max Wing Loading | |
Normal
Wing |
2626 kg
5789 lbs |
3664 kg
8077 lbs |
288.5 kg/m²
59 lbs/ft² |
Extended
Wing |
2692 kg
5934 lbs |
3730 kg
8223 lbs |
-
- |
Rate of Climb | Ceiling | Max. Endurance* | Max Range | Takeoff Run | Max Speed** | |
Normal
Wing |
18.4 m/sec
60.3 ft/sec |
11200 m
36750' |
1.26 hours | 870 km @ 11000 m
540 miles @ 36000' |
690 m
2263' |
931 km/h
578 mph |
Extended
Wing |
18.3 m/sec
60 ft/sec |
12100 m
39700' |
1.59 hours | 970 km @ 11800 m
602 miles @ 38700' |
635 m
2083' |
914 km/h
567 mph |
There are no scale models currently of any of these aircraft |
Above color image from: Luftwaffe Secret Projects: Fighters