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Helicopters - Prototypes 
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Airbus Helicopters H160M Guepard Multi-Mission Military Helicopter 2020
The H160M "Guepard" new-generation helicopter is a "medium twin" (medium-lift, twin-engine) militarized form of the original H160 X4 prototype helicopter developed by the French concern of Airbus Helicopters to satisfy the Joint Light Helicopter (JLH) program requirements of the French Armed Forces. The X4 took to the skies for the first time on June 13th, 2015 and was quickly marketed to interested parties thereafter. Offering a sleek appearance through fine design lines and skillful contouring, the platform gained interest from the French Armed Forces who preceded to adopt it through its M-model militarized form. The series is set for its own first flight in 2023 with deliveries to commence in 2026.

In French military service, the type is expected to stock the inventories of the French Army (80 examples), Navy (49 examples), and Air force (40 examples) - succeeding a collection of aging types in a broad collection of roles.

The H160M is developed with a "modular" mission set approach allowing the single airframe to be converted to fulfill a variety of over-battlefield roles. This includes general utility sorties as well as passenger transport, Search and Rescue (SAR), Medical Evacuation (MEDEVAC), and special forces support. Furthermore, the platform can be outfitted with pintle-mounted machine guns and sniper rifles as well as fuselage side-mounted machine guns (12.7mm HMP400 types) and anti-ship missiles to offer on-the-spot fire support services in the Close-Air Support (CAS) role for allied ground elements. Its versatility can also allow the helicopter to operate over-water in search for enemy vessels (to engage with missiles) or downed airmen. For the latter, the helicopter can be equipped with a powered winch system. An external cargo-carrying capability is also in-built, allowing sling loads.

The H160M sports such features as full-digital engine implementation, advanced cockpit and avionics, "Blue Edge" main rotor blades for reduced operating noises, a shrouded Fenestron tail rotor unit (further reducing noise levels), reduced maintenance requirements and maintenance costs over the life of the platform, and enhanced survivability.

Its overall configuration is highly conventional: the helicopter seats its crew of two in a side-by-side arrangement aft of a nose assembly. The positions are divided by a shared center console and vision out-of-the-cockpit is enhanced thanks to liberal use of windows offering elevated situational awareness. The cockpit front panel sports three large, full-color displays providing pertinent systems status and mission information. Conventional (redundant) control sticks and foot pedals will handle the helicopter's control scheme.

Under the radar-housing nose is a turreted Electro-Optical system. Ports along the fuselage sides offer pintle-mounted armament positions and, aft of this, is the passenger area complete with sliding fuselage doors. The engines are paired above the cabin roof in the usual way with the main rotor sitting close to the fuselage roof line. Exhaust ports for the engines blow upwards. The tail unit is elevated in the design and incorporates the typical elements such as rudder fin, horizontal tailplanes (the stabilizers being of a rather unique biplane design), and various antenna.

In French Army service, the H160M will be integrated into the battle command system in place that allows for unfettered support of active ground elements. Protected communications will allow information sharing with all involved parties to form a potent multi-pronged approach to engagements of enemy forces. For the French Navy, the helicopter will become a fixture of in-service warships, launched and retrieved from their decks and provide a critical over-the-horizon capability offering protection, airspace denial, rescue service, and an anti-ship capability. Shipboard storage will be aided by the main blades conveniently folding (manual acutation) rearwards over the tail. The French Air Force will benefit from the systems inherent versatility, providing SAR services as well as armed escort, fire support, and reconnaissance fulfillment.

At present, the design is set to take on a pair of pilots and seat five combat-ready infantry elements. Additional space is provided for the carrying of two stretchers. Power is set to be provided by 2 x Safran Arrano turboshaft engines promising excellent fuel efficiency. Maximum Take-Off Weight (MTOW) is set to reach 6,050 kilograms while range is out to 850 kilometers. Dimensions include a rotor diameter of 13.4 meters.
General characteristics
Crew: 2
Capacity: 12
Length: 14 m (45 ft 11 in)
Width: 12 m (39 ft 4 in)
Height: 4 m (13 ft 1 in)
Empty weight: 4,240 kg (9,348 lb)
Max takeoff weight: 5,670[20] kg (12,500 lb) extended gross weight: 6,050 kg (13,340 lb)
Max payload: 1,760 kg incl. up to 500 kg additional fuel
Powerplant: 2 × Turbomeca Arrano turboshaft engines
Main rotor diameter: 12 m (39 ft 4 in)

Performance
Maximum speed: 325 km/h (202 mph, 175 kn)
Cruise speed: 287 km/h (178 mph, 155 kn)
Range: 850 km (530 mi, 460 nmi)
Service ceiling: 5,900 m (19,357 ft)
Rate of climb: 8.9 m/s (1,750 ft/min)
The helicopter can be armed with MBDA’s Sea Venom (ANL) anti-ship missiles (ASMs) to perform anti-ship warfare missions. The over-the-horizon missile can engage targets within the range of 20km.

MBDA is developing Sea Venom/ANL, an helicopter-launched, over-the-horizon anti-ship weapon system, jointly funded by the UK and French Governments. It is the next generation multi-role surface attack weapon.

Capable of defeating the most challenging target set presented by today’s open water and littoral maritime operations, the new weapon features significant advances on both Sea Skua and AS15TT.

The new design will maintain some of the characteristics of Sea Skua and AS15TT and retain compatibility with existing logistic footprints, thereby allowing current users of these systems to upgrade easily.
Sea Venom/ANL offers:
Reduced modifications to existing ship storage and handling equipment
High helicopter load-out
Minimal impact on logistics and through-life costs
CALIBER: 7.62x51mm NATO
OPERATION: Open-bolt
WEIGHT: 22.9 lb.
BARREL LENGTH: 21.7″
OVERALL LENGTH: 41.6″
HEIGHT: 9″
RATE OF FIRE: 650 - 950 RPM
FN® HMP250/HMP400 Pod
SPECS (HMP250)
CALIBER: .50
MAG CAPACITY: Customer Specified
WEIGHT (EMPTY): 194 lb.
WEIGHT (LOADED): 257 lb.
HEIGHT: 16.1″
LENGTH: 71.3″
RATE OF FIRE: 950 - 1,100 RPM
SPECS (HMP400)
CALIBER: .50
MAG CAPACITY: Customer Specified
WEIGHT (EMPTY): 197 lb.
WEIGHT (LOADED): 305 lb.
HEIGHT: 17.1″
LENGTH: 76.4″
RATE OF FIRE: 950 - 1,100 RPM
H160M’s cockpit will accommodate up to two crew members. It will be equipped with the Helionix avionics suite, which integrates up to four multi-functional displays. FlytX is based on the Avionics 2020 concept unveiled at the 2013 Paris Air Show and comprises an intuitive touchscreen interface designed by pilots for pilots. Military helicopters are called on to perform reconnaissance, fire support, surveillance and search-and-rescue missions in increasingly saturated environments.

Pilots must be able to observe hostiles, evade obstacles and successfully complete their missions while flying the helicopter and monitoring information from its onboard systems. Fully mission-oriented, the FlytX solution has been developed to enable maximum efficiency. The technology used in FlytX is designed to reduce pilot workload, so that they can focus on their mission objective at every decisive moment. The spacious cabin offers an internal volume of more than 7m³ and can house up to 12 armed personnel.
2 x Safran Arrano turboshaft engine (Arrano 1A)

The H160 Guepard will be powered by two Safran Arrano turboshaft engines supplied by Safran Helicopter Engines. The engine will feature a two-stage centrifugal compressor, a reverse-flow combustion chamber, and a single-stage power turbine. It is expected to deliver a maximum power output of 1,300hp.
The 1A is the first variant of the Arrano, intended to power Airbus Helicopters’ revolutionary new twin-engine H160. In early 2015, Airbus Helicopters announced its decision to select the Arrano 1A as sole engine on the H160, in part, on its ability to deliver extra power when operating in hot-and-high conditions. The Arrano-powered H160 made its first flight on January 27, 2016.
The power-plant will reduce fuel consumption by 15% when compared to its counterparts and will also increase the payload-range performance of the H160M. The time between overhauls (TBO) of the Safran Arrano engine is 5,000 hours.