Specifications |
Contractors | Boeing McDonnell Douglas Helicopter Systems(Mesa, AZ)
General Electric (Lynn, MA)
Martin Marietta (Orlando, FL) |
Propulsion | Two T700-GE-701Cs |
Crew | Two |
| AH-64A | AH-64D |
Length | 58.17 ft (17.73 m) | 58.17 ft (17.73 m) |
Height | 15.24 ft (4.64 m) | 13.30 ft (4.05 m) |
Wing Span | 17.15 ft (5.227 m) | 17.15 ft (5.227 m) |
Primary Mission Gross Weight | 15,075 lb (6838 kg)
11,800 pounds Empty | 16,027 lb (7270 kg) Lot 1 Weight |
Hover In-Ground Effect (MRP) | 15,895 ft (4845 m)
[Standard Day]
14,845 ft (4525 m)
[Hot Day ISA + 15C] | 14,650 ft (4465 m)
[Standard Day]
13,350 ft (4068 m)
[Hot Day ISA + 15 C] |
Hover Out-of-Ground Effect (MRP) | 12,685 ft (3866 m)
[Sea Level Standard Day]
11,215 ft (3418 m)
[Hot Day 2000 ft 70 F (21 C)] | 10,520 ft (3206 m)
[Standard Day]
9,050 ft (2759 m)
[Hot Day ISA + 15 C] |
Vertical Rate of Climb (MRP) | 2,175 fpm (663 mpm)
[Sea Level Standard Day]
2,050 fpm (625 mpm)
[Hot Day 2000 ft 70 F (21 C)] | 1,775 fpm (541 mpm)
[Sea Level Standard Day]
1,595 fpm (486 mpm)
[Hot Day 2000 ft 70 F (21 C)] |
Maximum Rate of Climb (IRP) | 2,915 fpm (889 mpm)
[Sea Level Standard Day]
2,890 fpm (881 mpm)
[Hot Day 2000 ft 70 F (21 C)] | 2,635 fpm (803 mpm)
[Sea Level Standard Day]
2,600 fpm (793 mpm)
[Hot Day 2000 ft 70 F (21 C)] |
Maximum Level Flight Speed | 150 kt (279 kph)
[Sea Level Standard Day]
153 kt (284 kph)
[Hot Day 2000 ft 70 F (21 C)] | 147 kt (273 kph)
[Sea Level Standard Day]
149 kt (276 kph)
[Hot Day 2000 ft 70 F (21 C)] |
Cruise Speed (MCP) | 150 kt (279 kph)
[Sea Level Standard Day]
153 kt (284 kph)
[Hot Day 2000 ft 70 F (21 C)] | 147 kt (273 kph)
[Sea Level Standard Day]
149 kt (276 kph)
[Hot Day 2000 ft 70 F (21 C)] |
Range | 400 km - internal fuel
1,900 km - internal and external fuel |
Armament | M230 33mm Gun
70mm (2.75 inch) Hydra-70 Folding-Fin Aerial Rockets
AGM-114 Hellfire anti-tank missiles
AGM-122 Sidearm anti-radar missile
AIM-9 Sidewinder Air-to-Air missiles
|
Mission Equipment | Target Acquisition and Designation System /
Pilot Night Vision System |
Reliability | The general objective of aircraft readiness is to achieve 75% Mission Capable. |
Costs | |