General characteristics:
Crew: 3 (pilot, weapons system officer and technician)
Capacity: 8 troops or 4 stretchers
Length: 17.5 m (57 ft 4 in)
Rotor diameter: 17.3 m (56 ft 7 in)
Wingspan: 6.5 m (21 ft 3 in)
Height: 6.5 m (21 ft 3 in)
Disc area: 235 m² (2,530 ft²)
Empty weight: 8,500 kg (18,740 lb)
Max takeoff weight: 12,000 kg (26,500 lb)
Powerplant: 2× Isotov TV3-117VMA turbines, 1,600 kW (2,200 hp) each

Performance:
Maximum speed: 315 km/h
Range: 415 km
Service ceiling: 4,500 m (14,750 ft)

Armament:
flexible GSh-23-2 23mm double-barreled aircraft gun
fixed GSh-30K
PKT door mounted machine guns
8 x 9M114 Shturm Anti-Tank-rockets
2 x UB-32A-24 rocket launchers

Basic Information:

Series Designation: Sikorsky MH-53 Pave Low
Classification Type: Heavy-lift helicopter
Contractor: Sikorsky Aircraft
Status Active: 11 MH-53Js, 21 MH-53Ms
Reserve: 0
ANG: 0
Primary user: United States Air Force
Unit cost: MH-53J: US$40 million (2001 dollars)
Developed from: CH-53 Sea Stallion

Armament:
2 x 7.62mm machine guns

General characteristics:
Crew: 6 (two pilots, two flight engineers and two gunners)
Capacity: approx. 38 troops
Length: 88 ft (28 m)
Rotor diameter: 72 ft (21.9 m)
Height: 25 ft (7.6 m)
Empty weight: 32,000 lb (14,515 kg)
Max takeoff weight: 46,000 lb (50,000 lb in war time) (21,000 kg)
Powerplant: 2× General Electric T64-GE-100 turboshafts, 4,330 shp (3,230 kW) each
Rotor system: 6 blades

Performance:
Maximum speed: 165 mph (265 km/h) at sea level
Range: 600 nmi (1,100 km) ; Unlimited with aerial refueling
Service ceiling: 16,000 ft (4,900 m)

Type: Observation/scout helicopter
Manufacturer: Bell Helicopter Textron
Maiden flight: 8 December 1962[1]
Introduced: 1967
Status: Active service
Primary users: United States Army, Taiwan (Republic of China), Saudi Arabia
Produced: 1966-1989
Number built: 2,200+
Developed from: Bell 206

Specifications (OH-58D Kiowa Warrior):

General characteristics:
Crew: 2 pilots
Length: 40 ft 8 in (12.39 m)
Rotor diameter: 35 ft 0 in (10.67 m)
Height: 7 ft 6 in (2.29 m)
Empty weight: 3,290 lb (1,490 kg)
Max takeoff weight: 5,500 lb (2,495 kg)
Powerplant: 1× Rolls-Royce T703-AD-700A or 250-C30R/3 turboshaft, 650 eshp (485 kW)
Fuel capacity: 110 US gal (454 L)

Performance:
Maximum speed: 138 mph (222 km/h)
Cruise speed: 120 mph (195 km/h)
Range: 345 mi (556 km)
Service ceiling: 20,500 ft (6,250 m)
Rate of climb: 1,615 ft/min (8.2 m/s)

Armament:
AIM-92 Stinger air-to-air missiles in 2-round launchers

Operators:
Russia - Russian Air Force - 10 in service

Specifications (Mi-28A, 1987):

General characteristics:
Crew: 1 pilot (rear), 1 navigator/weapons operator (front)
Length: 17.01 m (55 ft 9 in)
Rotor diameter: 17.20 m (56 ft 5 in)
Height: 3.82 m (12 ft 7 in)
Empty weight: 8,095 kg (17,845 lb)
Loaded weight: 10,400 kg (22,930 lb)
Max takeoff weight: 11,500 kg (25,705 lb)
Powerplant: 2× Klimov TV3-117VMA turboshaft, 1,450 kW (1,950 hp) each

Performance:
Maximum speed: 300 km/h (187 mph)
Range: 1,100 km (640 mi)
Service ceiling: 5,800 m (19,000 ft)

Armament:
1x chin-mounted 30 mm Shipunov 2A42 cannon with 300 rounds (220° horizontal fire)
up to 2,300 kg of disposable stores on four hardpoints, including bombs, rockets, missiles, and gunpods

Type: Light utility helicopter
English name: Dolphin
Structure: Transmission manufactured by Dongan Engine Manufacturing Company at Harbin, hubs and tail rotor blades by Baoding Propeller Factory.
Power plant: TWO 547kW Turbomeca Arriel 1C1 turboshafts, produced by SAEC at Zhuzhou as WZ8A. From 2001, H410A powered by Arriel 2Cs as WZ8C. Fuel capacity 1,140 litres. Option for 180 litre auxiliary tank.
Armament: (WZ-9): Up to eight HJ-8 or HJ-8E ATMs (range 3 km); twin 12.7mm or 23mm gun pods; or two pods of 57 or 90mm rockets. Possible other weapons include TY-90 IR-guided AAM (already test- flown on Z-9 in 1998; range of 6 km) and C-701 TV-guided anti-ship missile (15 km).

Z-9C: Version for PLA Naval Air Force, for deployment aboard certain classes of destroyers and frigates; in service by late 2000. Believed to be equivalent to Arriel 2-engined Eurocopter AS 565 Panther, but equipped with Thales HS-12 dipping sonar and KLC-11/J-band (Chinese version of Agrion 15) surface search radar; armament includes two Yu-7 torpedoes or TV-guided C-701 anti-surface vessel missiles.

Basic Information:

Series Designation: Aerospatiale SA 341 / SA 342 Gazelle
Classification Type: Light Multi-Purpose Helicopter
Contractor: Aerospatiale - France / Westand - Britain
Country of Origin: France
Initial Year of Service: 1971
Crew / Accommodations: 2 + 3
Production Totals: 1,500*

Armament:
Available Hardpoints: 2 (with wing stubs)
Available Armament / Munitions:
Mission specific armament includes:
2 x Rocket Pods
4 or 6 x HOT anti-tank missiles
Mistal air-to-air missiles
Reconnaissance Pods
2 x 7.62mm machine guns
1 x 20mm Giat Cannon (starboard side)
2 x Surface-to-Air Missiles of Various makes.

Performance:
Powerplant: 1 x Turbomeca XIVM turboshaft engine delivering 640kW driving three blade main rotor and Fenestron shrouded tail rotor.
Maximum Speed: 165 miles per hour | 265 kilometers per hour | 143 knots
Maximum Range: 441 miles (710 km)
Service Ceiling: 1,532 feet | 467 meters | 0.3 miles
Initial Rate of Climb: 2,400 ft/min (731.5 m/min)

Dimensions:
Length: 31.27 feet (9.53 meters)
Wingspan/Width: 0.00 feet (0.00 meters)
Height: 10.43 feet (3.18 meters)
Empty Weight: 2,202 pounds (999 kilograms)
MTOW: 4,409 pounds (2,000 kilograms)