Specifications
Year: 2019
Status: In-Development
Manufacturer(s): Iran Helicopter Support and Renewal Company (PANHA) - Iran
Production: 1
Roles: Transport; VIP Transport; Search and Rescue (SAR); Reconnaissance (RECCE);
Status: In-Development
Manufacturer(s): Iran Helicopter Support and Renewal Company (PANHA) - Iran
Production: 1
Roles: Transport; VIP Transport; Search and Rescue (SAR); Reconnaissance (RECCE);
Crew: 1
Length: 37.40 ft (11.4 m)
Width: 36.91 ft (11.25 m)
Height: 10.50 ft (3.2 m)
Weight (Empty): 3,858 lb (1,750 kg)
Weight (MTOW): 6,393 lb (2,900 kg)
Length: 37.40 ft (11.4 m)
Width: 36.91 ft (11.25 m)
Height: 10.50 ft (3.2 m)
Weight (Empty): 3,858 lb (1,750 kg)
Weight (MTOW): 6,393 lb (2,900 kg)
Power: 2 x Turbomeca Arrius turboshaft engines developing 700 horsepower each and driving a four-bladed main rotor and two-bladed tail rotor.
Speed: 173 mph (278 kph; 150 kts)
Ceiling: 9,843 feet (3,000 m; 1.86 miles)
Range: 603 miles (970 km; 524 nm)
Rate-of-Climb: 1,750 ft/min (533 m/min)
Ceiling: 9,843 feet (3,000 m; 1.86 miles)
Range: 603 miles (970 km; 524 nm)
Rate-of-Climb: 1,750 ft/min (533 m/min)
Operators: Iran (possible)
The Saba-248 bears more than a passing resemblance to the Bell Helicopter Model 427, what essentially became a failed helicopter product for the American company (it only found two global users in the Czech Republic and Argentina). However, in the Iranian interpretation of this aircraft, the form and function of the Model 427 are all there. The helicopter showcases sleek contouring from nose-to-tail and the engine installations are well-embedded along the fuselage roof. The cockpit - featuring side-by-side seating and LCD displays - is aft of a short nosecone assembly. Entry/exit for the operating crew is by way of hinged automobile-style doors and larger rectangular doors allow access to the passenger cabin aft of the cockpit. All doors have large transparent screens and windows make up a large portion of the cockpit walls allowing for excellent vision and situational awareness. The tail section sports an elevated stem housing the drive shaft powering the tail rotor element. Vertical and horizontal planes are seated along the tail unit. The main rotor component consists of four total blades and the tail rotor - offset to portside - has two blades. The undercarriage is of a simple four-point skid arrangement.
Internally, the Saba-248 is made up largely of Western systems and subsystems. The engines are 2 x French-originated Turbomeca "Arrius" series turboshaft engines of 640 horsepower each. The gearbox is of Austrian origin. Altogether, the helicopter has an estimated top speed of 172.5 miles per hour putting it in line with Western helicopters of similar design and functionality.
A first-flight of a Saba-248 prototype was recorded in 2016. The Iranian military hopes to introduce the product into service sometime in 2019 following testing and certification prior to serial production efforts.
The Iranians plan to utility the Saba-248 series in several frontline roles including Search and Rescue (SAR). Its lightweight nature also opens it up for use as a reconnaissance platform and light-attack gunship.
Armament
Typically unarmed. Can be armed for the light gunship role with rocket pods, gun pods and cannon pods.
Variants / Models
• Saba-248 - Base Series Designation.
