Akaflieg Munchen Mü-13 Atalante / Merlin / Scheibe-Flugzeugbau Mü‑13E Bergfalke 1 / Schwarzwald Mü-13

Mü‑13D

One of the principal prewar German high performance designs, the single-seater Mü 13 was developed at the Munich Akaflieg from the two-seat Mü 10 Milan, which had been built there under the direction of Dipl-lng Egon Scheibe, who later formed, at the end of 1951, the sailplane firm bearing his name. The first single-seat Mü 13 flew in 1936. It has an all moving tailplane and DFS airbrakes for approach control.

There were a number of variants, some later having air brakes instead of flaps while the rear fuselage cross section was later changed from a rectangular one to triangular. The Mü 13D-3 of 1943 had an increased wing span, longer fuselage and a modified fin and rudder. In May 1939, Schmidt set a new German record for a goal flight of 482km (299 miles) in an Atalante. Unlike most sailplanes of its size the Mu 13 was of mixed construction, using steel and chrome-molybdenum-tin alloy as well as wood. The wooden cantilever wing had steel tube flaps and fabric-covered steel-framed ailerons while the fuselage was a fabric-covered steel framework of basically square cross-section and the tail unit of conventional wooden construction. Particular attention was paid to good visibility, there being large window panels inset into the sides of the cockpit while a clear panel inset into the wing centre section leading edge gave the pilot a better view above and behind him; the cockpit canopy was detachable, and several different shapes were used. A monowheel landing gear and tailskid were featured.

Scheibe built a development of the Mü 13 in Austria known as the Mü 13E Bergfalke (Mountain Falcon), which first flew in prototype form on 6 August 1951 and this two-seat general purpose glider went into production as the Scheibe Bergfalke. The original Mü 13 made its first flight in 1936 and the two prototypes were named the Merlin and the Atalante, differing from each other principally in the fuselage structure and control arrangements. The Atalante with a number of modifications was built by Kurt Schmidt at the Black Forest factory and about 150 Mü 13s were built in all.

Akaflieg Munchen Mü 13 Merlin
Span: 52 ft 6 in
Length: 19 ft 9 in
Wing area: 174 sq.ft
Aspect ratio: 15.85
Empty weight: 375 lb
Max weight: 595 lb
Max speed: 124 mph
Min sinking speed: 2 ft/sec at 34 mph
Best glide ratio: 28:1 at 41 mph

Mȕ 13 Atalante
Wing span: 16.0 m / 52 ft 6 in
Length: 6.02 m / 19 ft 9 in
Wing area: 16.16 sq.m / 174 sq ft
Wing section: Mil
Aspect ratio: 15.85
Empty weight: 170 kg / 375 lb
Max weight: 270 kg / 595 lb
Water ballast: None
Max wing loading: 16.71 kg/sq.m / 3.42 lb/sq ft
Max speed: 108 kt / 200 km/h
Stalling speed: 27 kt / 50 km/h
Min sinking speed: 0.6 m/sec / 2 ft/sec at 29.5 kt / 55 km/h
Best glide ratio: 28 at 35.5 kt / 66 km/h

Akaflieg Munchen Mü 13 D Atalante
Length: 19.783 ft / 6.03 m
Wingspan: 52.428 ft / 15.98 m
Crew: 1

Schwarzwald Mu-13 D
Wing span: 16 m
Wing area: 16.16 sq.m
Aspect ratio: 15.84
Airfoil: Mu-profil 15%
Empty Weight: 185 kg
Gross Weight: 275 kg
Wing Load: 17 kg/sq.m
L/DMax: 28 66 kph
MinSink: 0.60 m/s 55 kph
Seats: 1

Schwarzwald Mu 13D3
Wing span: 16 m / 52.5 ft
Wing area: 16.16 sq.m / 174 sq.ft
Aspect ratio: 15.85
Airfoil: Mu
Empty Weight: 170 kg / 375 lb
Payload: 100 kg / 220 lb
Gross Weight: 270 kg / 595 lb
Wing Load: 16.71 kg/sq.m / 3.42 lb/sq.ft
L/DMax: 25 66 kph / 35 kt / 40 mph
MinSink: 0.62 m/s / 2.0 fps / 1.18 kt
Seats: 1

Scheibe-Flugzeugbau Mü 13E Bergfalke 1
Length: 51.837 ft / 15.8 m
Wingspan: 56.43 ft / 17.2 m
Max take off weight: 551.3 lb / 250.0 kg
Crew: 2

Akaflieg Munchen Mü-11 Papagei

The Akaflieg München Mü11 Papagei is a primary glider that was designed and built at Akaflieg München in Germany in 1935.

The Mü11 Papagei, (Parrot), was a single-seat primary style training glider similar to the SG-38 but with a Mü Scheibe aerofoil section. Flight trials were carried out in 1935 but there is very little information available. Only one photograph and a contemporary model survive. The photograph shows the pilots seat surrounded by a plywood nacelle.

Akaflieg Munchen Mu-10 Milan

High Performance Glider, Germany, 1934
The Milan of 1934 was one of the first german, two-seater, high performance gliding airplanes. It had a steel tube frame and was developed by Egon Scheibe, who later became well known for glider design.

Length: 19.029 ft / 5.8 m
Wingspan: 58.399 ft / 17.8 m
Max take off weight: 407.9 lb / 185.0 kg
Max. speed: 65 kts / 120 km/h
Crew: 2

Akaflieg Karlsruhe AK-5

AK-5b

AK-5
Wing span: 15m
Wing area: 10.66sq.m
Empty Weight: 278kg
Gross Weight: 485kg
Wing Load: 45kg/sq.m
Aspect ratio: 21.11
Airfoil: HQ-21/17.5
Structure: GFRP
MinSink: 0.58 m/s @ 85 kph
L/DMax: 39 @ 105 kph
No. of Seats: 1
No. Built: 1

AK-5b
Wing span: 15m
Wing area: 10.66sq.m
Empty Weight: 255kg
Gross Weight: 450kg
Wing Load: 42.2kg/sq.m
Aspect ratio: 21.11
Airfoil: HQ-21/17,5
Structure: Glass, Carbon and Aramid
MinSink: 0,58 m/s at 85 km/h
L/DMax: max 39 at 105 km/h
No. of Seats: 1

Akaflieg Darmstadt D-39

This unique single-seat powered sailplane, created by the Darmstadt Akaflieg, looks exactly like a Standard Class high-performance sailplane except for its low-mounted wing. It features a retractable two-blade folding propeller, driven by twin Fichtel & Sachs modified KM 914V engines situated in the nose cone.

The D-39 is an adaptation of the basic D-38 airframe, having the same glassfibre/balsa sandwich construction with ailerons of glassfibre/Klegecel foam sandwich, and Schempp-Hirth airbrakes on the upper wing surfaces. No flaps are fitted. It is equipped with a manually-retractable sprung monowheel, and accommodation comprises a semi-reclining seat under a flush canopy, the rear section of which is detachable.

The D-39 first flew on 28 June 1979.

Engine: Limbach 68 PS
Wing span: 17.5m
Wing area: 13.4sq.m
Empty Weight: 438kg
Gross Weight: 563kg
Wing Load: 40kg/sq.m
Aspect ratio: 22.9
Airfoil: FX 61-184
Structure: GFRP
L/DMax: 37 @ 100 kph
MinSink: 0.70 m/s @ 87 kph
No. of Seats: 1
No. Built: 1

D-39
Engines: 2 x Fichtel & Sachs KM 914V, 35 kW (47 hp)
Wing span: 15.0 m / 49 ft 2 in
Length: 7.15 m / 23 ft 5.5 in
Height: 1.02 m / 3 ft 4.5 in
Wing area: 11.0 sq.m / 118.4 sq ft
Wing section: Wortmann FX-61 -184/60-126
Aspect ratio: 20.5
Empty weight: 280 kg / 617 lb
Max weight: 400 kg / 882 lb
Water ballast: None
Max wing loading: 36.3 kg/sq.m / 7.43 lb/sq ft
Max speed: 135 kt / 250 km/h
Stalling speed: 39 kt / 72 km/h
Min sinking speed: 1.0 m/sec / 3.3 ft/sec
Best glide ratio: 36 at 56.5 kt / 105 km/h
T-O run: 200 m / 656 ft
Rate of climb at S/L: 240 m/min / 787 ft/min
Range: 500 km / 269 nm