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AH-64A/D Apache Attack Helicopter, USA
Key Data:
Crew: 2 - pilot and copilot / gunner
Dimensions: Main Rotor Blade Diameter 14,630cm
Height 3,590cm
Empty Weight 5,352kg
Performance: Maximum Cruising Speed 260km/h
Maximum Rate of Climb 942m/min
Maximum Vertical Rate of Climb 474m/min
Range 400km on internal fuel 1,900km on internal and external fuel
Endurance 3hrs 9min on internal fuel
g Limit Values +3.5g to -0.5g
Featured Suppliers:
BEI Precision Systems & Space Company - Optical Encoders, Scanners and Accelerometers
Data Device Corporation - High-Reliability Data Networking Technology, COTS Products and Subsystems
Honeywell-LMB - Fans and Motors for Aerospace and Defence Applications
Kappa opto-electronics - Day and Night Sight Systems, Barrel Inspection, Marksmen Training and X-Ray Detection
MS Kennedy Corporation - Custom Hybrids, Motor Drives and Power Modules for Army Aircraft and Weapons Systems
Parvus Corp - Rugged COTS Embedded Computer and Network Subsystems
TDI Power - Robust Power Supplies for Military Applications
Eurocopter/Tiger Attack Helicopter, Germany & France
Dimensions:
Length 14m
Height 3.81m
Wingspan 13m
Design Mission Weight 5,400kg
Alternate Gross Weight 6,000kg
Weapons:
Trigat Missile Range 500m to 5km
Maximum Air-to-Air Missile Range Over 5km autonomously
Target Identification and Engagement 5km
Performance:
Hover Out of Ground Effect
Multi-role version - 3,200m
Combat support version - 3,500m
Vertical Rate of Climb
Multi-role version - 5.2m/sec
Combat support version - 6.4m/sec
Maximum Rate of Climb
Multi-role version - 10.7m/sec
Combat support version - 11.5m/sec
Flight Speed, Armed
Multi-role version - 145kt
Combat support version - 155kt
Cruise Speed
124kt
Design Limit Speed
Multi-role version - 161kt
Combat support system - 174kt
Maximum Range, Internal Fuel
800km
Mission Endurance
2 hours 50 minutes
Maximum Endurance, Internal Fuel
3 hours 25 minutes
Agility
40º angle of yaw after first second
Fuel Capacity:
Maximum Internal Fuel 1,020kg
Maximum Internal and External Fuel 1,575kg
Featured Suppliers:
Data Device Corporation - High-Reliability Data Networking Technology, COTS Products and Subsystems
ESG - Command, Control and Information Systems
ATAK T-129, Turkey
Specifics
Crew: 2 pilots
Length: 14.6 m (47 ft 11 in)
Rotor diameter: 11.90 m (39 ft 0 in)
Height: 3.4 m (11 ft 2 in)
Disc area: 444.9 m² (4,789 ft²)
Max takeoff weight: 5,000 kg (11,023 lb) Powerplant: 2× LHTEC CTS800-4A turboshaft, 1,014 kW (1,361 shp) each Propellers: five blade rotor
Performance
Cruise speed: 269 km/h (145 knots, 167 mph)
Range: 561 km (303 nm, 341 mi)
Ferry range: 1,000 km (540 nm, 620 mi)
Armament
Guns: 1× 20 mm (0.787 in) three-barrel gatling-type cannon (500 rounds)
Rockets: 4 pods with
38× 81 mm (3.19 in) unguided rockets or
76× 70 mm (2.75 in) unguided rockets or
12.7 mm machine gun-pod
Missiles: 8× AGM-114 Hellfire, BGM-71 TOW, Hydra 70, Spike-ER anti-tank missiles and Sura D/Snora.
4-8× AIM-92 Stinger or Mistral or AIM-9 Sidewinder anti-aircraft missiles
AH-1 Super Cobra, US
Dimensions:
Length 13.9m
Height 4.02m
Rotor Diameter 14.63m
Weights:
Empty Weight 12,200lb (10,920lb)
Maximum Gross Weight 16,800lb (14,750lb)
Internal Fuel 2,755lb (2,086lb)
Maximum Ordnance 3,914lb (1,661lb)
Hovering Out of Ground Effect (HOGE) Gross Weight 16,600lb (10,300lb)
Engines:
Powerplant 2 x General Electric T700-401 rated at 1,625shp
Performance:
Maximum Airspeed 210kt (170kt)
Cruise Speed at Altitude 3,000ft and 91.5°F 210kt (170kt)
Cruise Speed at Altitude 4,000ft and 95°F 137kt (131kt)
Maximum Range With 20 Minutes Reserve Fuel 350nm
Endurance With 20 Minutes Reserve Fuel 3hr 30min (2h 48min)
Maximum G-load +3.2g (+2.5g)
Minimum G-load -0.5g (+0.5g)
Vertical Rate of Climb at Altitude 3,000ft 1,740ft/min (645ft/min)
Vertical Rate of Climb at Altitude 4,000ft 1,386ft/min (315ft/min)
Featured Suppliers:
Data Device Corporation - High-Reliability Data Networking Technology, COTS Products and Subsystems
AH-2 Rooivalk, South Africa
Key Data:
Crew Pilot, weapon systems officer
Missions Anti-armour, ground suppression, anti-helicopter, ferry, reconnaissance and counter-insurgency
Dimensions:
Main Rotor to Tail Rotor 18,732mm
Main Rotor Diameter 15,580mm
Overall Height 5,187mm
Weights: Maximum Take-Off Weight 8,750kg
Minimum Operating Weight 5,730kg
Maximum Internal Fuel 1,469kg
Engines:
Powerplant 2 x Makila 1K2
Twin-Engine Take-Off Rating 2,243kW
Single-Engine, Super Continence 1,660kW
Performance: Fast Cruise Speed 150kt
Maximum Sideways Speed 50kt
Maximum Rate of Climb, Twin-Engine Operation 2,620ft/min
Maximum Rate of Climb, Single-Engine Operation 1,280ft/min
Maximum Range, Internal Fuel 700km
Maximum Range, External Fuel 1,280ft/min
Maximum Hover Ceiling (OGE) Out-of-Ground Effect 17,900ft
Maximum Hover Ceiling (IGE) In-Ground Effect 19,200ft
Excess Hover Power margin OGE, Sea-Level Anti-Tank Mission 39%
Armament:
Missiles 8 or 16 anti-tank missiles, 7in SAL missile or HOT3
Air-to-air missiles, infrared guidance Rockets
38 or 76 70mm unguided rockets, variation of warheads
Cannon 20mm F2 cannon, high-velocity ammunition (900 rounds)
Sighting Systems: Dual Helmet-Mounted Sight and Display (HMSD)
Stabilised nose-mounted sight with FLIR, TV, laser rangefinder, laser designator and autotracking
Avionics:
Total mission modes
Target acquisition
Flight control
Health and usage monitoring
Communications
Threat detection and control
Flight and fuel
Featured Suppliers:
Honeywell-LMB - Fans and Motors for Aerospace and Defence Applications
Sources:
Army Technology
T129 | AgustaWestland
Key Data:
Crew: 2 - pilot and copilot / gunner
Dimensions: Main Rotor Blade Diameter 14,630cm
Height 3,590cm
Empty Weight 5,352kg
Performance: Maximum Cruising Speed 260km/h
Maximum Rate of Climb 942m/min
Maximum Vertical Rate of Climb 474m/min
Range 400km on internal fuel 1,900km on internal and external fuel
Endurance 3hrs 9min on internal fuel
g Limit Values +3.5g to -0.5g
Featured Suppliers:
BEI Precision Systems & Space Company - Optical Encoders, Scanners and Accelerometers
Data Device Corporation - High-Reliability Data Networking Technology, COTS Products and Subsystems
Honeywell-LMB - Fans and Motors for Aerospace and Defence Applications
Kappa opto-electronics - Day and Night Sight Systems, Barrel Inspection, Marksmen Training and X-Ray Detection
MS Kennedy Corporation - Custom Hybrids, Motor Drives and Power Modules for Army Aircraft and Weapons Systems
Parvus Corp - Rugged COTS Embedded Computer and Network Subsystems
TDI Power - Robust Power Supplies for Military Applications
Eurocopter/Tiger Attack Helicopter, Germany & France
Dimensions:
Length 14m
Height 3.81m
Wingspan 13m
Design Mission Weight 5,400kg
Alternate Gross Weight 6,000kg
Weapons:
Trigat Missile Range 500m to 5km
Maximum Air-to-Air Missile Range Over 5km autonomously
Target Identification and Engagement 5km
Performance:
Hover Out of Ground Effect
Multi-role version - 3,200m
Combat support version - 3,500m
Vertical Rate of Climb
Multi-role version - 5.2m/sec
Combat support version - 6.4m/sec
Maximum Rate of Climb
Multi-role version - 10.7m/sec
Combat support version - 11.5m/sec
Flight Speed, Armed
Multi-role version - 145kt
Combat support version - 155kt
Cruise Speed
124kt
Design Limit Speed
Multi-role version - 161kt
Combat support system - 174kt
Maximum Range, Internal Fuel
800km
Mission Endurance
2 hours 50 minutes
Maximum Endurance, Internal Fuel
3 hours 25 minutes
Agility
40º angle of yaw after first second
Fuel Capacity:
Maximum Internal Fuel 1,020kg
Maximum Internal and External Fuel 1,575kg
Featured Suppliers:
Data Device Corporation - High-Reliability Data Networking Technology, COTS Products and Subsystems
ESG - Command, Control and Information Systems
ATAK T-129, Turkey
Specifics
Crew: 2 pilots
Length: 14.6 m (47 ft 11 in)
Rotor diameter: 11.90 m (39 ft 0 in)
Height: 3.4 m (11 ft 2 in)
Disc area: 444.9 m² (4,789 ft²)
Max takeoff weight: 5,000 kg (11,023 lb) Powerplant: 2× LHTEC CTS800-4A turboshaft, 1,014 kW (1,361 shp) each Propellers: five blade rotor
Performance
Cruise speed: 269 km/h (145 knots, 167 mph)
Range: 561 km (303 nm, 341 mi)
Ferry range: 1,000 km (540 nm, 620 mi)
Armament
Guns: 1× 20 mm (0.787 in) three-barrel gatling-type cannon (500 rounds)
Rockets: 4 pods with
38× 81 mm (3.19 in) unguided rockets or
76× 70 mm (2.75 in) unguided rockets or
12.7 mm machine gun-pod
Missiles: 8× AGM-114 Hellfire, BGM-71 TOW, Hydra 70, Spike-ER anti-tank missiles and Sura D/Snora.
4-8× AIM-92 Stinger or Mistral or AIM-9 Sidewinder anti-aircraft missiles
AH-1 Super Cobra, US
Dimensions:
Length 13.9m
Height 4.02m
Rotor Diameter 14.63m
Weights:
Empty Weight 12,200lb (10,920lb)
Maximum Gross Weight 16,800lb (14,750lb)
Internal Fuel 2,755lb (2,086lb)
Maximum Ordnance 3,914lb (1,661lb)
Hovering Out of Ground Effect (HOGE) Gross Weight 16,600lb (10,300lb)
Engines:
Powerplant 2 x General Electric T700-401 rated at 1,625shp
Performance:
Maximum Airspeed 210kt (170kt)
Cruise Speed at Altitude 3,000ft and 91.5°F 210kt (170kt)
Cruise Speed at Altitude 4,000ft and 95°F 137kt (131kt)
Maximum Range With 20 Minutes Reserve Fuel 350nm
Endurance With 20 Minutes Reserve Fuel 3hr 30min (2h 48min)
Maximum G-load +3.2g (+2.5g)
Minimum G-load -0.5g (+0.5g)
Vertical Rate of Climb at Altitude 3,000ft 1,740ft/min (645ft/min)
Vertical Rate of Climb at Altitude 4,000ft 1,386ft/min (315ft/min)
Featured Suppliers:
Data Device Corporation - High-Reliability Data Networking Technology, COTS Products and Subsystems
AH-2 Rooivalk, South Africa
Key Data:
Crew Pilot, weapon systems officer
Missions Anti-armour, ground suppression, anti-helicopter, ferry, reconnaissance and counter-insurgency
Dimensions:
Main Rotor to Tail Rotor 18,732mm
Main Rotor Diameter 15,580mm
Overall Height 5,187mm
Weights: Maximum Take-Off Weight 8,750kg
Minimum Operating Weight 5,730kg
Maximum Internal Fuel 1,469kg
Engines:
Powerplant 2 x Makila 1K2
Twin-Engine Take-Off Rating 2,243kW
Single-Engine, Super Continence 1,660kW
Performance: Fast Cruise Speed 150kt
Maximum Sideways Speed 50kt
Maximum Rate of Climb, Twin-Engine Operation 2,620ft/min
Maximum Rate of Climb, Single-Engine Operation 1,280ft/min
Maximum Range, Internal Fuel 700km
Maximum Range, External Fuel 1,280ft/min
Maximum Hover Ceiling (OGE) Out-of-Ground Effect 17,900ft
Maximum Hover Ceiling (IGE) In-Ground Effect 19,200ft
Excess Hover Power margin OGE, Sea-Level Anti-Tank Mission 39%
Armament:
Missiles 8 or 16 anti-tank missiles, 7in SAL missile or HOT3
Air-to-air missiles, infrared guidance Rockets
38 or 76 70mm unguided rockets, variation of warheads
Cannon 20mm F2 cannon, high-velocity ammunition (900 rounds)
Sighting Systems: Dual Helmet-Mounted Sight and Display (HMSD)
Stabilised nose-mounted sight with FLIR, TV, laser rangefinder, laser designator and autotracking
Avionics:
Total mission modes
Target acquisition
Flight control
Health and usage monitoring
Communications
Threat detection and control
Flight and fuel
Featured Suppliers:
Honeywell-LMB - Fans and Motors for Aerospace and Defence Applications
Sources:
Army Technology
T129 | AgustaWestland