Leonardo AW249

Dedicated Twin-Seat, Twin-Engine Attack Helicopter [ 2025 ]

The AW249 is an in-development attack helicopter project headed by Leonardo of Italy which has partnered with PGZ of Poland.

Authored By: Staff Writer | Last Edited: 02/18/2021 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

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There has been relatively little advancement in the field of the dedicated attack helicopter platform with primary, globally-operated, types in the Boeing AH-64 Apache and Mil Mi-24 Hind both being born in the Cold War period (1947-1991). Even the Russian Army, operating two attack helo types in the Mil Mi-28 Havoc and Kamov Ka-50 Black Shark series, use platforms rooted in the Cold War years when tanks were to rule the battlefields of Europe. The Italian Army operates the Agusta A129 Mangusta but even this product emerged during the 1980s. More recent efforts has resulted in the Eurocopter Tiger, introduced in 2003 but fewer than 150 being built, and the T129 ATACK from Turkey - though this is based in the Italian A129 platform. The U.S. Marines has introduced a heavily upgraded form of the classic Bell AH-1 Huey Cobra line in the "Viper" series.

As such, it is of great interest that Leonardo of Italy has announced an all-new development venture with its "AW249". The aircraft is set to follow tried-and-proven design practices for helicopters by included a twin, side-by-side engine arrangement for maximum power and survivability, a stepped cockpit configuration for pilot and gunner, and rugged, fixed tail-dragging undercarriage. Concept artwork reveals a platform set to carry a chin-mounted, trainable automatic cannon and port and starboard side wingstubs for ordnance (three hardpoints to a wing). Over the fuselage is a low-mounted, five-bladed main rotor while the tail is set to feature a starboard-side-facing four-bladed tail rotor unit to counter torque. The fuselage is depicted with smooth, angled panels.

Leonardo SpA was granted a 487 million Euro deal in January of 2017 for the development of four aircraft encompassing a single flyable prototype and three pre-production forms.

Requirements by any army service for their attack helicopter platforms has not changed - survivability is key for both crew and aircraft alike so stealth measures will be implemented into the new August product by way of reduced radar cross-section and low-signature engines.

To help drive development, the Italian Army has insisted on utilization of some in-service components such as a 20mm TM197B autocannon by OTO-Melara for the chin weapon, the Israeli SPIKE Anti-Tank Guided Missile (ATGM) family for the anti-tank measure, and the main rotor and gearbox of the Agusta AW149 medium-lift helicopter series. Beyond this, the turboshaft installations for power would be either the proven American-originated General Electric CT7-2E1 or the French Safran "Aneto" currently employed in the Leonardo AW189K model - both set to offer output power in the 2,000 horsepower range.©MilitaryFactory.com

Other estimated specifications include a Maximum Take-Off Weight (MTOW) of up to 17,640lb, a cruising speed of just over 160 miles per hour, a mission endurance window of up to three hours and an operating service ceiling reaching 20,000 feet.

Leonardo has stated that its new combat helicopter will incorporate many lessons learned in the design, development, manufacture and sustainment of its A129. Communications will be broadened to provide integration (namely command and control) for Unmanned Aerial Vehicles (UAVs). The redesigned wingstubs will offer six hardpoints for various ordnance types over the traditional four placements seen in modern attack helicopters of this class and support both Air-to-Air and Air-to-Ground weapons. Reduced pilot workload will figure into the cockpit as will an all-modern Battle Management System (BMS). The twin engine arrangement, while improving survivability, will allow for operation over land (including "Hot-and-High" environments) and water, giving the AW249 a maritime quality often inherently lacking in attack helicopter designs.

For the Italian Army, the AW249 would immediately succeed its aging fleet of A129 Mangusta helicopters and the global approach to the development of the new helicopter would no doubt reel in foreign supporters - possibly Poland and Turkey, both of whom will be seeking replacements for their own dedicated attack helicopter fleets by the late 2020s, early 2030s. In fact, Poland is an early target of the AW249 project and Leonardo has inked a collaborative partnership with Polska Grupa Zbrojeniowa (PGZ Group) of Poland for just that. The two concerns have been in talks since 2016 with several deals inked from that year until now. Poland has the active "Kruk" procurement program to cover acquisition of a new combat helicopter.

Italian Army A129 helicopters are expected to face retirement concerns as soon as 2026 capping what would be over 35 years of consistent, reliable operation for the service. The new challenge will be to adopt a product that could see another healthy 35 year service life - one that is easily adaptable for close-support battles as well as armed escort and anti-armor sorties. For the Poles, an advanced tank-killer is a considerable need - namely due to recent aggressions seen by Russia in Ukraine and its forceful takeover of Crimea.©MilitaryFactory.com

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March 2019 - The AW249 is in the running to satisfy a Japanese Defense requirement for a New Attack Helicopter (NAH).

February 2021 - It has been announced that the CT7 turboshaft engine from General Electric will power the in-development AW249 attack helicopter. The specific engine mark will be the CT7-8E6 rated at 2,500 horsepower.

Specifications

Service Year

2025

Origin

Italy

Status

IN-DEVELOPMENT
Program in Progress.

Crew

2

Production

0
UNITS

Leonardo SpA - Italy / PGZ Group - Poland

(View other Aviaton-Related Manufacturers)

Italy (possible); Poland (possible); Turkey (possible)

(OPERATORS list includes past, present, and future operators when applicable)

GROUND ATTACK
Ability to conduct aerial bombing of ground targets by way of (but not limited to) guns, bombs, missiles, rockets, and the like.

CLOSE-AIR SUPPORT
Developed to operate in close proximity to active ground elements by way of a broad array of air-to-ground ordnance and munitions options.

INTELLIGENCE-SURVEILLANCE-RECONNAISSANCE
Surveil ground targets / target areas to assess environmental threat levels, enemy strength, or enemy movement.

Length

41.0 ft
(12.50 m)

Width/Span

39.4 ft
(12.00 m)

Height

11.0 ft
(3.35 m)

Empty Wgt

9,921 lb
(4,500 kg)

MTOW

17,637 lb
(8,000 kg)

Wgt Diff

+7,716 lb
(+3,500 kg)

(Showcased structural values pertain to the base Leonardo AW249 production variant)

Installed: 2 x General Electric CT7-8E6 turboshaft engines developing 2,500 horsepower each driving a five-bladed main rotor and four-blade tail rotor.

Max Speed

174 mph
(280 kph | 151 kts)

Ceiling

19,685 ft
(6,000 m | 4 mi)

Range

342 mi
(550 km | 297 nm)

Rate-of-Climb

2,050 ft/min
(625 m/min)

♦ MACH Regime (Sonic)

Sub

Trans

Super

Hyper

HiHyper

ReEntry

♦

(Showcased performance specifications pertain to the base Leonardo AW249 production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)

PROPOSED:
1 x 20mm OTO-Melara TM197B rotary cannon in turreted chin position.

OPTIONAL:
Mixed ordnance loads to include guided-missiles and precision-guided/unguided rockets/pods across six total wingstub hardpoints.

Supported Types

Graphical image of an aircraft automatic cannon

Graphical image of an aircraft Gatling-style rotating gun

Graphical image of aircraft aerial rockets

Graphical image of an aircraft guided bomb munition

(Not all ordnance types may be represented in the showcase above)

6
Hardpoints

AW249 - Base Series Designation.

General Assessment

Firepower

Performance

Survivability

Versatility

Impact

Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.

Overall Rating

The overall rating takes into account over 60 individual factors related to this aircraft entry.

34

Rating is out of a possible 100 points.

Relative Maximum Speed

Hi: 200mph

Lo: 100mph

This entry's maximum listed speed (174mph).

Graph average of 150 miles-per-hour.

City-to-City Ranges

NYC

LON

PAR

BER

MOS

TOK

SYD

LAX

NYC

Operational range when compared to distances between major cities (in KM).

Max Altitude Visualization

Design Balance

The three qualities reflected above are altitude, speed, and range.

Aviation Era Span

Showcasing era cross-over of this aircraft design.

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