A-10 Thunderbolt II
General characteristics
- Crew: 1
- Length: 53 ft 4 in (16.26 m)
- Wingspan: 57 ft 6 in (17.53 m)
- Height: 14 ft 8 in (4.47 m)
- Wing area: 506 ft² (47.0 m²)
- Airfoil: NACA 6716 root, NACA 6713 tip
- Empty weight: 24,959 lb (11,321 kg)
- Loaded weight: 30,384 lb (13,782 kg)) On CAS mission: 47,094 lb (21,361 kg)
On anti-armor mission: 42,071 lb (19,083 kg - Max takeoff weight: 50,000 lb (23,000 kg)
- Powerplant: 2× General Electric TF34-GE-100A turbofans, 9,065 lbf (40.32 kN) each
- Never exceed speed: 450 knots (518 mph,[88] 833 km/h) at 5,000 ft (1,500 m) with 18 Mk 82 bombs[89]
- Maximum speed: 381 knots (439 mph, 706 km/h) at sea level, clean[88]
- Cruise speed: 300 knots (340 mph, 560 km/h)
- Stall speed: 120 knots (138 mph, 220 km/h) [90]
- Combat radius:
- On CAS mission: 250 nmi (288 mi, 460 km) at 1.88 hour single-engine loiter at 5,000 ft (1,500 m), 10 min combat
- On anti-armor mission: 252 nmi (290 mi, 467 km), 40 nm (45 mi, 75 km) sea-level penetration and exit, 30 min combat
- Ferry range: 2,240 nmi (2,580 mi, 4,150 km) with 50 knot (55 mph, 90 km/h) headwinds, 20 minutes reserve
- Service ceiling: 45,000 ft (13,700 m)
- Rate of climb: 6,000 ft/min (30 m/s)
- Wing loading: 99 lb/ft² (482 kg/m²)
- Thrust/weight: 0.36
- Guns: 1× 30 mm (1.18 in) GAU-8/A Avenger gatling cannon with 1,174 rounds
- Hardpoints: 11 (8× under-wing and 3× under-fuselage pylon stations) with a capacity of 16,000 lb (7,260 kg) and provisions to carry combinations of:
- Rockets:
- 4× LAU-61/LAU-68 rocket pods (each with 19× / 7× Hydra 70 mm rockets, respectively)
- 4× LAU-5003 rocket pods (each with 19× CRV7 70 mm rockets)
- 6× LAU-10 rocket pods (each with 4× 127 mm (5.0 in) Zuni rockets)
- Missiles:
- 2× AIM-9 Sidewinders air-to-air missiles for self-defense
- 8× AGM-65 Maverick air-to-surface missiles
- Bombs:
- Mark 80 series of unguided iron bombs or
- Mk 77 incendiary bombs or
- BLU-1, BLU-27/B Rockeye II, Mk20, BL-755[91] and CBU-52/58/71/87/89/97 cluster bombs or
- Paveway series of Laser-guided bombs or
- Joint Direct Attack Munition (A-10C)[92] or
- Wind Corrected Munitions Dispenser (A-10C)
- Other:
- SUU-42A/A Flares/Infrared decoys and chaff dispenser pod or
- AN/ALQ-131 & AN/ALQ-184 ECM pods or
- Lockheed Martin Sniper XR & LITENING targeting pods (A-10C) or
- 2× 600 US gallon Sargent Fletcher drop tanks for extended range/loitering time.
- Rockets:
- AN/AAS-35(V) Pave Penny laser tracker pod[93] (mounted beneath right side of cockpit) for use with Paveway LGBs
- Head-up display (HUD) for improved technical flying and air-to-ground support.[94]
Rockwell B-1 Lancer
- Crew: 4 (aircraft commander, copilot, offensive systems officer and defensive systems officer)
- Payload: 125,000 lb (56,600 kg) ; internal and external ordnance combined
- Length: 146 ft (44.5 m)
- Wingspan:
- Extended: 137 ft (41.8 m)
- Swept: 79 ft (24.1 m)
- Height: 34 ft (10.4 m)
- Wing area: 1,950 ft² (181.2 m²)
- Airfoil: NA69-190-2
- Empty weight: 192,000 lb (87,100 kg)
- Loaded weight: 326,000 lb (148,000 kg)
- Max takeoff weight: 477,000 lb (216,400 kg)
- Powerplant: 4× General Electric F101-GE-102 augmented turbofans
- Dry thrust: 14,600 lbf (64.9 kN) each
- Thrust with afterburner: 30,780 lbf (136.92 kN) each
- Fuel capacity, optional: 10,000 U.S. gal (38,000 L) fuel tank for 1–3 internal weapons bays each
- Maximum speed:
- At altitude: Mach 1.25 (721 knots, 830 mph, 1,340 km/h at 50,000 ft/15,000 m altitude)
- At low level: Mach 0.92 (700 mph, 1,130 km/h at 200–500 ft/60-150 m altitude)
- Range: 6,478 nmi (7,456 mi, 11,998 km)
- Combat radius: 2,993 nmi (3,445 mi, 5,543 km)
- Service ceiling: 60,000 ft (18,000 m)
- Wing loading: 167 lb/ft² (816 kg/m²)
- Thrust/weight: 0.38
- Hardpoints: six external hardpoints for 50,000 lb (22,700 kg) of ordnance and 3 internal bomb bays for 75,000 lb (34,000 kg) of ordnance.
- Bombs:
- 84× Mk-82 AIR inflatable retarder general purpose bombs
- 81× Mk-82 low drag general purpose bombs
- 84× Mk-62 Quickstrike sea mines
- 24× Mk-65 naval mines
- 30× CBU-87/89/CBU-97 Cluster Bomb Units (CBU)
- 30× CBU-103/104/105 Wind Corrected Munitions Dispenser
- 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
- 12× AGM-154 Joint Standoff Weapon
- 96× or 144× GBU-39 Small Diameter Bomb GPS guided bombs (not fielded on B-1 yet)
- 24× AGM-158 JASSM
- 24× B61 thermonuclear variable-yield gravity bombs
- 24x B83 nuclear bomb
- 1× AN/APQ-164 forward-looking offensive passive phased-array radar
- 1× AN/ALQ-161 radar warning and defensive jamming equipment
- 1× AN/ASQ-184 defensive management system
- 1× Lockheed Martin Sniper XR targeting pod (optional)[145][146]
F-22A Raptor
General characteristics
- Crew: 1
- Length: 62 ft 1 in (18.90 m)
- Wingspan: 44 ft 6 in (13.56 m)
- Height: 16 ft 8 in (5.08 m)
- Wing area: 840 ft² (78.04 m²)
- Airfoil: NACA 64A?05.92 root, NACA 64A?04.29 tip
- Empty weight: 43,430 lb (19,700 kg[2][190])
- Loaded weight: 64,460 lb (29,300 kg[191])
- Max takeoff weight: 83,500 lb (38,000 kg)
- Powerplant: 2× Pratt & Whitney F119-PW-100 Pitch Thrust vectoring turbofans
- Dry thrust: 23,500 lb[192] (104 kN) each
- Thrust with afterburner: 35,000+ lb[2][192] (156+ kN) each
- Fuel capacity: 18,000 lb (8,200 kg) internally,[2][190] or 26,000 lb (11,900 kg) with two external fuel tanks[2][190]
- Maximum speed:
- At altitude: Mach 2.25 (1,500 mph, 2,410 km/h)[87]
- Supercruise: Mach 1.82 (1,220 mph, 1,963 km/h)[87]
- Range: 1,600 nmi (1,840 mi, 2,960 km) with 2 external fuel tanks
- Combat radius: 410 nmi[189] (471 mi, 759 km)
- Ferry range: 2,000 mi (1,738 nmi, 3,219 km)
- Service ceiling: 65,000 ft (19,812 m)
- Wing loading: 77 lb/ft² (375 kg/m²)
- Thrust/weight: 1.08 (1.26 with loaded weight & 50% fuel)
- Maximum design g-load: -3.0/+9.0 g[87]
- Guns: 1× 20 mm (0.787 in) M61A2 Vulcan gatling gun in starboard wing root, 480 rounds
- Air to air loadout:
- Air to ground loadout:
- 2× AIM-120 AMRAAM and
- 2× AIM-9 Sidewinder for self-protection, and one of the following:
- 2× 1,000 lb (450 kg) JDAM or
- 2× Wind Corrected Munitions Dispensers (WCMDs) or
- 8× 250 lb (110 kg) GBU-39 Small Diameter Bombs
- Hardpoints: 4× under-wing pylon stations can be fitted to carry 600 US gallon drop tanks or weapons, each with a capacity of 5,000 lb (2,268 kg).[193][194]
Multi-Mission UAV
General Characteristics
- Crew: None
- Landing Type: runway
- Launch Type: runway
- Length: 36 ft (11 m)
- Wingspan: 66 ft (20 m)
- Height: 12.5 ft (3.6 m)
- Empty weight: 4,900 lb (2223 kg)
- Fuel Capacity: 4,000 lb (1,800 kg)
- Max takeoff weight: 10,500 lb (4760 kg)
- Power Plant: Honeywell TPE331-10 turboprop engine, 900 shp (671 kW), with Digital Electronic Engine Control (DEEC)[59]
- Maximum speed: 260 knots (482 km/h, 300 mph)
- Cruise speed: 150–170 knots (276–313 km/h, 172–195 mph)[60]
- Range: 3,200 nmi (5,926 km, 3,682 mi)
- Endurance: 14–28 hours (14 hours fully loaded)[61]
- Payload: 3,800 lb (1,700 kg)
- Internal: 800 lb (360 kg)
- External: 3,000 lb (1,400 kg)
- Service ceiling: 50,000 ft (15 km)
- Operational altitude: 25,000 ft (7.5 km)[62]
- 7 Hardpoints
- Up to 14 AGM-114 Hellfire air to ground missiles can be carried or four Hellfire missiles and two 500 lb (230 kg) GBU-12 Paveway II laser-guided bombs. The 500 lb (230 kg) GBU-38 Joint Direct Attack Munition (JDAM) can also be carried. Testing is underway to support the operation of the AIM-92 Stinger air-to-air missile.
