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https://en.wikipedia.org/wiki/Henschel_Hs_129
The Henschel Hs 129 was a World War II ground-attack aircraft fielded by the German Luftwaffe. The aircraft saw combat in Tunisia and on the Eastern Front By the mid-1930s, the German military, as well as its counterparts in other countries, had come to see the main role of ground-attack aircraft as the interdiction of logistics and materiel, a task in which targets were often poorly protected and less likely to be protected by strong, well-coordinated defences. For high-value, well-protected tactical targets dive bombers had become the conventional solution. However, the experience of the German Kondor Legion during the Spanish Civil War (1936–39) refuted this idea. Even though it was equipped with types unsuited to the role, such as the Henschel Hs 123 and cannon-armed versions of the Heinkel He 112, the Kondor Legion proved that ground-attack aircraft were a very effective weapon. This led to support within the Luftwaffe for the creation of an aircraft dedicated to this role, and the Reichsluftministerium (RLM; "Reich Air Ministry") requested tenders for a specialized ground attack aircraft. It was anticipated that the main source of damage to such an aircraft would be small arms fire from the ground, meaning that the plane had to be well-armored around its cockpit and engines. Similar protection was also needed in the canopy, in the form of 75 mm (2.95 in) thick armored glass. The aircraft was expected to be attacking in low-level, head-on strafing runs, so the cockpit had to be located as close as possible to the nose, in order to maximize the visibility of its targets. Another, non-operational, requirement severely hampered the designs: the RLM insisted that the new design be powered by engines that were not being used in existing aircraft, so that the type would not interfere with production of established types deemed essential to the war effort. The Hs 129 was designed around a single large "bathtub" of steel sheeting that made up the entire nose area of the plane, completely enclosing the pilot up to head level. Even the canopy was steel, with only tiny windows on the side to see out of and two angled blocks of glass for the windscreen. In order to improve the armor's ability to deflect bullets, the fuselage sides were angled in forming a triangular shape, resulting in almost no room to move at shoulder level. There was so little room in the cockpit that the instrument panel ended up under the nose below the windscreen where it was almost invisible; some of the engine instruments were moved outside onto the engine nacelles' inboard-facing surfaces, as on some models of Messerschmitt's Bf 110 heavy fighter, and the gunsight was mounted outside on the nose. Henschel's plane came in 12% overweight with the engines 8% underpowered, and understandably, it flew poorly. The controls proved to be almost inoperable as speed increased, and in testing, one plane flew into the ground from a short dive because the joystick forces were too high for the pilot to pull out. The Focke-Wulf design proved to be no better. Both planes were underpowered with their air-cooled, inverted-V12 Argus As 410 engines, and very difficult to fly. The RLM nevertheless felt they should continue with the basic concept. The only real deciding factor between the two designs was that the Henschel was smaller and cheaper. The Focke-Wulf was put on low priority as a backup, and testing continued with the Hs 129 A-0. A series of improvements resulted in the Hs 129 A-1 series, armed with two 20 mm MG 151/20 cannons and two 7.92 mm (.312 in) MG 17 machine guns, along with the ability to carry four 50 kg (110 lb) bombs under the fuselage centreline. Role Ground-attack Manufacturer Henschel First flight 25 May 1939 Introduction April 1942 Retired 1945 Primary users Luftwaffe Hungarian Air Force Romanian Air Force Produced June 1940 – September 1944 Number built 865 B-1s started rolling off the lines in December 1941, but they were delivered at a trickle. In preparation for the new plane, I./SchlG 1 had been formed up in January with Bf 109 E/Bs (fighter-bomber version of Bf 109 E) and Hs 123s, and they delivered B-0s and every B-1 that was completed. Still, it was not until April that 12 B-1s were delivered and the 4th staffel (squadron) became ready for action. They moved to the Eastern Front (to the Crimea) in the middle of May 1942, and in June they received a new weapon, the 30 mm (1.2 in) MK 101 cannon with armor-piercing ammunition in a centerline pod. Specifications (Hs 129 B-2) General characteristics Crew: one, pilot Length: 9.75 m (31 ft 11¾ in) Wingspan: 14.20 m (46 ft 7 in) Height: 3.25 m (10 ft 8 in) Wing area: 29.0 m² (312.15 ft²) Empty weight: 4,020 kg (8,860 lb) Max. takeoff weight: 5,250 kg (11,574 lb) Powerplant: 2 × Gnome-Rhône 14M 4/5 14-cylinder radial engines, 522 kW (700 hp) each Performance Maximum speed: 407 km/h (220 knots, 253 mph) at 3,830 m (12,570 ft) (clean) Range: 690 km (372 nmi, 428 mi) Service ceiling: 9,000 m (29,530 ft) Rate of climb: 8.1 m/s (1,595 ft/min) Armament 2 x 7.92 mm (0.31 in) MG-17 machine guns, later models from 1943 to 1944 replaced the MG-17s with 2 x 13 mm (.51 in) MG 131 machine guns 2 x 20 mm MG 151/20 cannons 4 x 50 kg (110 lb) fragmentation bombs on belly racks or a 30 mm (1.2 in) MK 101 armor-piercing gun in a conformally mounted gun pod. Later models could also carry a MK-103 gun pod, or a BK-3.7 gun pod. 2 x 50 kg bombs on underwing mounts * |
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