Air Power Series>1:72 die-cast display model>A-10>HA1310
A-10A Thunderbolt II 25th Fighter Sqn "Assam Draggins",Osan, Dec. 2005
General Background
A-10 was the first USAF aircraft designed specifically for “Close Air Support ” (CAS) . It can be described as the outcome of the experience gained in the Vietnam War and the threats of the Soviet Union armor forces during the Cold War era. The first A-10A “Thunderbolt II” was delivered October 1975 and deployment in March 1976.
A-10's pilot is protected by titanium armor around his seat and the canopy isa large bubble canopy which provides all-round vision. The aircraft is designed with dual engines and the self-sealing fuel cells are protected by internal and external foam . Extra titanium is used to protect some flight control system parts of the aircraft. All these insure the plane and pilot's safety from enemy fires.
A-10's pilot is protected by titanium armor around his seat and the canopy isa large bubble canopy which provides all-round vision. The aircraft is designed with dual engines and the self-sealing fuel cells are protected by internal and external foam . Extra titanium is used to protect some flight control system parts of the aircraft. All these insure the plane and pilot's safety from enemy fires.
The Aircraft
On Oct. 1, 1993, the 25th Fighter Squadron was activated under the
51st Wing at Osan AB, Republic of Korea, under the command of Lt. Col.
Syd McPherson. It has since added six A-10 aircraft to its fleet,
making it a dual qualified A/OA-10 squadron. The 25th Fighter Squadron
Assam Draggins remain the premier close air support fighter squadron
on the Korean Peninsula today.
Specifications :
| Crew : | One |
| Main role : | A-10 - close air support, OA-10 - airborne forward air control |
| Manufacturer : | Fairchild Republic Co. |
| Power Plants : | Two General Electric TF34-GE-100 turbofans |
| Thrust : | 9,065 pounds per engine |
| Length : | 16.16 meters |
| Height : | 4.42 meters |
| Wingspan : | 17.42 meters Speed: 420 miles per hour (Mach 0.56) |
| Ceiling : | 13,636 meters |
| Maximum Takeoff Weight : | 22,950 kg. |
| Range : | 800 miles (695 nautical miles) |
| Armament : | One 30 mm GAU-8/A seven-barrel Gatling gun (fixed) |
| Maximum 7,200 kg of mixed ordnance including : 225 kg “ Mk-82 ” and 900 kg “ Mk-84 ” series low/high drag bombs, incendiary cluster bombs, combined effects munitions, mine dispensing munitions, AGM-65 Maverick missiles and laser-guided/electro-optically guided bombs , infrared countermeasure flares , electronic countermeasure chaff , jamming pods , 6.99 cm (2.75in.) rockets , illumination flares , AIM-9 Sidewinder missiles |