General characteristics:
Loaded weight: 737 kg
Cruising speed: 282 km/h
Range: 513 km

General characteristics:
Length: 44,50 meters
Wingspan: 41,80 meters
Loaded weight: 148.000 kg
Maximum speed: 1517 km/h
Engine: 4× General Electric F101-GE-102 augmented turbofans
Range: 11998 km

Armament:
Hardpoints: six external hardpoints for 59,000 lb (27,000 kg) of ordnance (use for weapons currently restricted by START I treaty) and 3 internal bomb bays for 75,000 lb (34,000 kg) of ordnance to carry from:

Missiles:
24× AGM-158 JASSM
12× AGM-154 JSOW

Bombs:
84× Mk-82AIR inflatable retarder general purpose bombs
81× Mk-82 low drag general purpose bombs
84× Mk-62 Quickstrike sea mines
8× Mk-65 naval mines
30× CBU-87/89/CBU-97 Cluster Bomb Units (CBU)
30× CBU-103/104/105 WCMD
24× GBU-31 JDAM GPS guided bombs
15× GBU-38 JDAM GPS guided bombs (Mk-82 general purpose warhead)
24× Mk-84 general purpose bombs
96× or 144× GBU-39 Small Diameter Bomb GPS guided bombs
16x B61 thermonuclear variable-yield gravity bombs

General characteristics:
Length: 19,20 meters
Wingspan: 11,70 meters
Loaded weight: 26.300 kg
Cruising speed: 2417 km/h
Engine: 2 TL General Electric J79-GE-17
Range: 2200 km

General characteristics:
Length: 47,72 meters
Wingspan: 56,39 meters
Loaded weight: 221 t
Cruising speed: 1010 km/h
Engine: 8 P & W TF33-P-3
Range: 20150 km

General characteristics:
Loaded weight: 500 kg
Cruising speed: 250 km/h
Range: 150 km

General characteristics:
Length: 19,82 meters
Wingspan: 28,60 meters
Loaded weight: 19.731 kg
Cruising speed: 291 km/h
Engine: two Pratt & Whitney R-2800-CA3 mit je 1.566 kW
Range: 2430 km

General characteristics:
Length: 8.14 meters 26 feet 8 inches
Wingspan: 12.7 meters 41 feet 8 inches
Loaded weight: 1020 kg 2,250 lb
Cruising speed: 130 km/h 81 mph / 70 kt
Service ceiling: 7,600 meters 25,000 feet
Endurance: 24+ hours

Armament:
6 hard points, 2 of which can carry drop tanks.
up to 6 AGM-114 Hellfire (MQ-1A)
or up to 2 250lb iron bombs and 4 other lighter weapons
or up to 6 AIM-92 Stinger (unknown number) (MQ-1A)
or some combination of the previous.

Type: Light utility aircraft
Manufacturer: Cessna Aircraft Company
Maiden flight: 1967
Introduced: 1968
Produced: 1968-1978
Number built: 4,295

General characteristics:
Crew: 1 pilot
Capacity: 3 passengers
Length: 27 ft 8 in (8.44 m)
Wingspan: 35 ft 6 in (10.82 m)
Height: 8 ft 7 in (2.62 m)
Wing area: 174 ft² (16.2 m²)
Empty weight: 1,495 lb (680 kg)
Max takeoff weight: 2,500 lb (1,100 kg)
Powerplant: 1× Lycoming O-360-A1F6D flat-4 engine, 180 hp (135 kW)

Performance:
Maximum speed: 136 knots (157 mph, 250 km/h)
Cruise speed: 124 knots (143 mph, 230 km/h)
Range: 604 nm (695 mi, 1,120 km)
Service ceiling: 14,600 ft (4,450 m)
Rate of climb: 840 ft/min (4.27m/s) 

Type: Interceptor/multi-role Fighter aircraft
Manufacturer: Grumman
Designed by Bob Kress, engineering manager
Maiden flight: 21 December 1970
Introduction: September 1974
Retired: 22 September 2006, USN
Status: Active service with Iran
Retired from US service
Primary users: United States Navy
Islamic Republic of Iran Air Force
Number built: 712
Unit cost: US$38 million in 1998

General characteristics:
Crew: 2 (Pilot and Radar Intercept Officer)
Length: 62 ft 9 in (19.1 m)
Wingspan: Spread: 64 ft (19.5 m), Swept: 38 ft (11.58 m)
Height: 16 ft (4.88 m)
Wing area: 565 ft² (54.5 m²)
Airfoil: NACA 64A209.65 mod root, 64A208.91 mod tip
Empty weight: 43,735 lb (19,838 kg)
Loaded weight: 61,000 lb (27,700 kg)
Max takeoff weight: 74,350 lb (33,720 kg)
Powerplant: 2× General Electric F110-GE-400 afterburning turbofans
Dry thrust: 13,810 lbf (61.4 kN) each
Thrust with afterburner: 27,800 lbf (124.7 kN) each

Performance:
Maximum speed: Mach 2.34 (1,544 mph, 2,485 km/h) at high altitude
Combat radius: 500 nm (575 mi, 926 km)
Ferry range: 1,600 nm (1,840 mi, 2,960 km)
Rate of climb: >45,000 ft/min (229 m/s)
Wing loading: 113.4 lb/ft² (553.9 kg/m²)
Thrust/weight: 0.91

Armament - 13,000 lb (5,900 kg) of ordnance including:
Guns: 1× M61 Vulcan 20 mm Gatling Gun
Missiles: AIM-54 Phoenix, AIM-7 Sparrow, AIM-9 Sidewinder air-to-air
Loading configurations:
2× AIM-9 + 6× AIM-54
2× AIM-9 + 2× AIM-54 + 4× AIM-7
2× AIM-9 + 4× AIM-54 + 2× AIM-7
2× AIM-9 + 6× AIM-7
4× AIM-9 + 4× AIM-54
4× AIM-9 + 4× AIM-7
Bombs: GBU-10, GBU-12, GBU-16, GBU-24, GBU-24E Paveway I/II/III LGB, GBU-31, GBU-38 JDAM, Mk-20 Rockeye II, Mk-82, Mk-83 and Mk-84 series iron bombs

Avionics:
Hughes AN/APG-71 radar
AN/ASN-130 INS, IRST, TCS

Type: Business jet
Manufacturer: Dassault Aviation
Maiden flight: 1 December 1970
Introduction: 1971
Number built: 226
Developed from: Dassault Falcon 20

General characteristics:
Crew: 2
Capacity: 4-8
Length: 13.86 m (45 ft 5.75 in)
Wingspan: 13.08 m (42 ft 11 in)
Height: 4.61 m (15 ft 1.5 in)
Wing area: 24.1 m² (259.42 ft²)
Empty weight: 4880 kg (10760 lb)
Gross weight: 8500 kg (18740 lb)
Powerplant: 2 × Garrett TFE731-2 turbofans, 1465 kN (3230 lbf) thrust each each

 
Performance:
Cruising speed: 912 km/h (566 mph)
Range: 3560 km (2212 miles)

Type: Fixed-wing gunship
Manufacturer: Lockheed and Boeing
Maiden flight: 1966, AC-130A
1990, AC-130U
Introduction: 1968, AC-130A
1995, AC-130U
Status: Active
Primary user: U.S. Air Force
Number built 43, including all variants
Unit cost: US$132.4 million (AC-130H)
US$190 million (AC-130U) in 2001