Intended to replace the Gloster Meteor F.Mk 4s in service with the Argentine air force, the I.Ae.33 Pulqui II (Arrow II) was designed by a team headed by Dr Kurt Tank, roughly inspired by the Ta 183. Tank arrived in Argentina in 1947, not speaking Spanish but with the plans for the German project TA-83 from the factory Focke Wulf. The first plane that Tank made in Argentina was a copy of the TA-83 which was his starting point.
It embodied some of the results of the advanced research carried out in Germany during World War II, incorporating a shoulder-mounted wing with 40deg of sweep-back, and a T-tail with all-swept surfaces. Landing gear was retractable tricycle-type and power provided by a Rolls-Royce Nene turbojet mounted in the rear fuselage. The pilot was accommodated on an ejection-seat in a pressurised cockpit, protected by armour and a bulletproof windscreen, and a sliding canopy that could be jettisoned in emergency, and auto pilot.
By 1950 the first prototype of the Pulqui II was ready for testing. It was piloted for the first time by Captain Edmundo Weiss on June 27, 1950.
Captain Edmundo Weiss is with the Pulqui II
It had its official debut on February 8, 1951. Tank called Peron in Buenos Aires from Cordoba and advised him that the airplane would arrive to the airport before the President himself. Sure enough, he was correct. During the presentation ceremony Peron expressed his admiration and gratitude for Tank.
The Pulqui II’s first tragedy occurred in May of that year after 28 test flights when a defect caused the death of Captain Vedania Mannuwal, a fighter pilot. This led to the third prototype and many more test flights. Two days before the newest version was to be presented to Peron in October of 1952, another crash cost the life of Otto Behrens who was an important part of the entire process. (Otto Behrens, the test pilot died; a few days before his death he said that the airplane was “the worst he had ever experienced as a test pilot”). His death was mourned by the entire country, especially the Germans now working in Argentina. By 1953 the fourth prototype was ready for testing. It was not until 18 September 1959 that the last was flown.
Unfortunately, just when the project was ready to bear fruit, a coup turned the country upside down. Many of the scientist and engineers associated with the project were forced from the country, including Kurt Tank. The new government showed little interest in keeping the project alive, although those who remained struggled to make it work. In a desperate attempt to change momentum, FMA planned a high profile test flight from Cordoba to Moron back to Cordoba including three quick rounds over the Buenos Aires airport, without supplementary fuel tanks. The pilot, Captain Rogelio Balado, was able to make the entire trip, but a fault in the system caused a lack of oxygen for him and he crashed on landing in Cordoba.
In 1954 a world tour was planned to exhibit the airplane to possible buyers. FMA also received visitors from the USSR, US (from the company that manufactured the P-86 Sabre) and Egypt who were interested in the airplane.
Brigadier Ahrens from the Argentina Air Force approached FMA requesting an estimate on the fabrication of 100 Pulquis. He was advised that 10 could be available immediately and that number 100 would be finished within 5 years. Ahrens decided to give the contract to the Americans for 100 F-86 Sabres because they would be available immediately. This basically ruined FMA’s future possibilities to export the Pulqui II.
In the intervening period the Dr Tank and his team had left Argentina. These factors, coupled with serious financial problems, meant that development was initially halted in 1953, and finally cancelled with the fall of Peron in 1955.
I.Ae.33 Engine; 1 x Rolls-Royce Nene, 2268kg Wingspan; 10.60 m / 34 ft 9 in Length; 11.68 m / 38 ft 4 in Height; 3.50 m / 11 ft 6 in Wing area; 25.10 sq.m / 270.17 sq ft Max take-off weight; 5550 kg / 12236 lb Empty weight; 3600 kg / 7937 lb Max. speed; 1050 km/h / 652 mph Ceiling; 15000 m / 49200 ft Crew; 1 Armament; 4 x 20mm cannon
Engine; 1 x 155hp Blackburn Cirrus Major Wingspan; 10.70 m / 35 ft 1 in Length; 8.12 m / 27 ft 8 in Height; 2.18 m / 7 ft 2 in Wing area; 16.50 sq.m / 177.60 sq ft Max take-off weight; 981 kg / 2163 lb Empty weight; 750 kg / 1653 lb Max. speed; 230 km/h / 143 mph Cruise speed; 195 km/h / 121 mph Ceiling; 5180 m / 17000 ft Range; 1570 km / 976 miles Crew; 2
Engine; 1 x 150hp Blackburn Cirrus Major Wingspan; 10.37 m / 34 ft 0 in Length; 7.95 m / 26 ft 1 in Height; 1.90 m / 6 ft 3 in Wing area; 16.00 sq.m / 172.22 sq ft Max take-off weight; 916 kg / 2019 lb Empty weight; 635 kg / 1400 lb Max. speed; 240 km/h / 149 mph Cruise speed; 210 km/h / 130 mph Ceiling; 6500 m / 21350 ft Crew; 2
Engine; 2 x 850hp Rolls-Royce Merlin 604 Wingspan; 15.00 m / 49 ft 3 in Length; 11.52 m / 38 ft 10 in Height; 5.16 m / 17 ft 11 in Wing area; 35.32 sq.m / 380.18 sq ft Max take-off weight; 7600 kg / 16755 lb Empty weight; 6208 kg / 13686 lb Max. speed; 740 km/h / 460 mph Cruise speed; 500 km/h / 311 mph Ceiling; 8000 m / 26250 ft Range; 2700 km / 1678 miles Crew; 1 Armament; 6 x 20mm cannon, 250kg of bombs
Designed by Emile Dewoitine, the I.Ae.27 Pulqui (Arrow) was the first single-seat fighter to be designed in Argentina as well as the first turbojet-powered aircraft to be built and flown in Argentina.
A cantilever low-wing monoplane of all-metal construction, the Pulqui had a conventional tail unit, retractable tricycle landing gear, and accommodation for the pilot well forward on the fuselage beneath a jettisonable canopy. Power was provided by a Rolls-Royce Derwent turbojet mounted in the aft fuselage. First flown on 9 August 1947, the Pulqui performance was well below estimates and development was abandoned.
I.Ae.27 Engine; 1 x Rolls-Royce Derwent, 1633kg Wingspan; 11.25 m / 36 ft 11 in Length; 9.69 m / 31 ft 9 in Height; 3.39 m / 11 ft 1 in Wing area; 19.70 sq.m / 212.05 sq ft Max take-off weight; 3600 kg / 7937 lb Empty weight; 2358 kg / 5199 lb Max. speed; 720 km/h / 447 mph Ceiling; 15500 m / 50850 ft Range; 900 km / 559 miles Crew; 1 Armament; 1 x 20mm cannon
Length; 14.70 m / 48 ft 3 in Height; 3.84 m / 13 ft 7 in Wing area; 79.10 sq.m / 851.42 sq ft Empty weight; 2460 kg / 5423 lb Wingspan; 25.50 m / 84 ft 8 in Max. speed; 220 km/h/ 137 mph Crew; 1 Passengers; 16
Engine; 2 x 1050hp Pratt & Whitney R-1830-G Twin Wasp Wingspan; 16.30 m / 54 ft 6 in Length; 12.00 m / 39 ft 4 in Height; 3.62 m / 12 ft 11 in Wing area; 38.12 sq.m / 410.32 sq ft Max take-off weight; 7200 kg / 15873 lb Empty weight; 5340 kg / 11773 lb Max. speed; 440 km/h / 273 mph Cruise speed; 410 km/h / 255 mph Ceiling; 10000 m / 32800 ft Range; 1200 km / 746 miles Armament; 4 x 12.7mm machine-guns or 4 x 20mm cannon, 800kg of bombs Crew; 2
Engine; 1 x 140hp Siemens Sh 14A Wingspan; 9.00 m / 30 ft 6 in Length; 7.30 m / 24 ft 11 in Height; 2.72 m / 9 ft 11 in Wing area; 20.00 sq.m / 215.28 sq ft Max take-off weight; 860 kg / 1896 lb Empty weight; 500 kg / 1102 lb Max. speed; 188 km/h / 117 mph Cruise speed; 160 km/h / 99 mph Ceiling; 4200 m / 13800 ft Range; 720 km / 447 miles Crew; 2
The first airplane designed by the Institute Aviation, and first counting on an Argentine engine. It flew for the first time the 8 of August of 1944 commanded by the Lieutenant First Osvaldo Rovere. Two series of 100 units each were ordered by the Commando of Military aviation; in 1946 the first series was completed and in 1950, the second. A monoplane of cantilever low-mounted wing, its construction was totally in native wood from the province of Missions. The fuselage was of semimonocoque structure of oval section. The stabilizer covered in wood and rudder in linen cloth. A conventional undercarriage retractable towards the center, operating electrically or manually, with hydraulic brakes. The cockpit with tandem seats, acrylic cover; the forward with a height restriction. The Ae 16 GAUCHO 9 cylinders radial offered 450 hp at 2200 r.p.m. with a mixed wood FMA prop initially, later a metal two-blade Hamilton Standard 2M-D30 of variable pitch. An Armstrong Siddeley Cheetah radial of 475 hp with a two-blade Rotol constant speed propeller was fitted to a version designated I.Ae.22-C. Initially used as an advanced trainer with dual controls, the armament included two fixed Madsen machine guns of 7.65 mm with 450 rounds each. An observation model has a movable machine gun in the rear position and carried three bombs of 50 kg and six rockets of 11 kg each.
Engine; 1 x 450hp Ae.16 Gaucho Wingspan; 12.60 m / 41 ft 4 in Length; 9.20 m / 30 ft 2 in Height; 2.84 m / 9 ft 4 in Wing area; 23.19 sq.m / 249.61 sq ft Max take-off weight; 2200 kg / 4850 lb Empty weight; 1520 kg / 3351 lb Max. speed; 290 km/h / 180 mph Cruise speed; 226 km/h / 140 mph Ceiling; 6000 m / 19700 ft Range; 1100 km / 684 miles Crew; 2