Arsenal J 36 Falke

J 36 Falke
Melasian J 36 Falke with a started engine on an advanced airfield near Humboldtsberg in 1942
Role	Fighter aircraft
National origin	Melasia
Manufacturer	Arsenal
Designer	Erich Krammer
First flight	10 April 1938
Introduction	1939
Retired	1961 Melasian air force
Status	Retired
Primary user	Melasian air force
Produced	1939–1946
Number built	227 + 3 prototypes
Variants	Arsenal J 42 Arsenal J 49

The J 36 Falke (hawk) was a Melasian fighter aircraft of the first half of the 20th century. It was designed by Erich Krammer and produced by the Melasian aviation company Arsenal. The aircraft is remarkable for being Melasia's first domestically designed and produced fighter aircraft and the first non-Berean type of combat aircraft to exceed speeds of 400 km/h (200 kn) in a straight level flight. The J 36 was of a mixed semi-monocoque and stressed skin design, built mostly of wood and fabric, with metal used in vital points of the structure like the engine cowling and the rudder fin joint. It also had some advanced features for the period, like the retractable landing gear, the completely enclosed cockpit and the split flaps. The high wingspan and the short fuselage provided a relatively small wing loading, while the light weight of the wooden construction coupled with a powerful V-12 engine allowed for a respectable degree of manoeuvrability.

The J 36 was a result of a fear in high echelons of Melasian government of possible Berean sanctions due to the aggressive Melasian foreign policy in Kenlong and against Mascylla. A tender was called for a lightweight fighter aircraft to replace the aging endargered Melasian air fleet, that consisted of mostly Mascyllary-built machines. The Melasian Ministry of war called for an aircraft equipped with the Lavarian-built Fábrica Automotiva Popular 12Y engine and the Nordic 20mm Oerlikon FF gun, both available after an agreemend was signed between Melasia and the respectable countries earlier 1936. Following a short public tender the variant presented by Arsenal was selected. The aircraft was introduced in 1939 and relatively quickly became the standard Melasian fighter. It served actively during the Melasian Crisis, when it proved to be a potent opponent to earlier Mascyllary aircraft on low altitudes. After the initial stages of the conflict, and the introduction of newer models by the Mascyllary air force, the J 36 began to underperform and was almost withdrawn from frontline service when the conflict seized in 1943. The remaining inventory of J 36s was then used in Kenlong, where it performed anti-guerrilla operations against the various Kenlongese revolutionary groups. The type was withdrawn from frontline service with the Melasian air force in 1949 but remained in the inventory up until the early 1960s.

The J 36 served only with the Melasian air force, although several airframes were transported to Mascylla for evaluation during the Melasian crisis. The slow production rate and the ever-growing international isolation of the country prevented its international export potential, with several states showing interest prior to the crisis being rejected by the Melasian government due to lack of surplus aircraft engines. Several attempts to improve and upgrade the model were performed throughout its service life, with the J 49 seeing the most success and becoming the next standard Melasian fighter.

Design

Description of the J 36 in the Fallish Encyclopedia of 20th century aircraft

Operators

Melasia

• Melasian Air Force operated the type since its introduction in 1939 up until 1961, and used it in the Melasian crisis and during the Kenlongese civil war

Mascylla

• Several aircraft were captured during the Melasian Crisis and shipped to Mascylla for evaluation and trials

Specifications

3-view drawing of J 36 Serie 1 Falke

Data from The J 36 type certification sheet

General characteristics

• Crew: 1
• Length: 7.40 m (24 ft 3 in)
• Wingspan: 9.36 m (30 ft 9 in)
• Height: 2.57 m (8 ft 5 in)
• Wing area: 16 m² (170 sq ft)
• Airfoil: NACA 63(2)-615
• Empty weight: 1,360 kg (2,998 lb)
• Max takeoff weight: 2,460 kg (5,423 lb)
• Fuel capacity: 440 kg (520 L avgas)
• Powerplant: 1 × Fábrica Automotiva Popular 12Y V-12 liquid-cooled piston engine
  

619 kW (830 hp) for take-off at 2,520 rpm at sea level

567 kW (760 hp) rated power at 2,400 rpm at sea level

641 kW (860 hp) rated power at 2,400 rpm at 3,150 m (10,335 ft)

• Specific fuel consumption: 0.265 kg/kWh (0.436 lb/(hp⋅h))
• Specific oil consumption: 0.008 kg/kWh (0.013 lb/(hp⋅h))

• Propellers: 3-bladed variable-pitch propeller, 3 m (9 ft 10 in) diameter
  

Performance

• Maximum speed: 442 km/h (275 mph; 239 kn) at 1,500 m (4,900 ft)
• Cruise speed: 380 km/h (236 mph; 205 kn) at 1,500 m (4,900 ft)
• Stall speed: 120 km/h (75 mph; 65 kn) without flaps
• Range: 820 km (510 mi; 443 nmi) at 66% power
• Combat range: 600 km (373 mi; 324 nmi)
• Endurance: 2 hours 30 minutes (average combat mission)
• Service ceiling: 8,000 m (26,000 ft)
• Time to altitude:
  

5,000 m (16,404 ft) in 8 minutes 46 seconds

• Wing loading: 154 kg/m² (32 lb/sq ft)
• Power/mass: 2.95 kg/kW (4.85 lb/hp)
• Take-off run to 8 m (26 ft): 320 m (1,050 ft)
• Landing run from 8 m (26 ft): 420 m (1,378 ft)

Armament

• Guns:
  

• 1× 20 mm (0.787 in) Oerlikon FF cannon (60 rounds)
• 2× 7.92 mm (0.312 in) MG 17 machine guns (500 rpg)

See also

Related development
Arsenal J 42
Arsenal J 49

Further reading

• [J 36 preliminary design calculations]