Hs 121
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- Hs 121 Fighter and advanced flight training aircraft
- First flight: 1934
- Henschel
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The Hs.121 was designed to one of the first specifications issued by the so-called C-amt, the technical department of Goering's commissariat. These specifications were for a "home defense fighter" - a dual-purpose aircraft for advanced flight training and a light fighter. Another green company among its competitors had three of the most experienced aviation firms in Germany - Arado, Focke-Wulf and Heinkel. Purely aesthetically, the Henschel version was the most attractive - Koch emphasized aerodynamic qualities.
One could feel the strong influence of Zygmunt Puławski from PZL, who in the early 30s brought Poland to the forefront in the field of fighter aircraft - Nikolaus chose the same "gull" strut scheme. The semi-elliptical light alloy wing had two spars and a metal-sheathed nose, followed by fabric lining. The oval fuselage had a set of metal spars and spars. The lining in the bow was metal, and in the cockpit area it was also working. The flaps went from the aileron to the fuselage. All steering surfaces were covered with cloth. The main landing gear with oil damping was attached to the first frame. Chassis wheels were covered with fairings. Like its competitors, the Hs.121 was equipped with an Argus As-10C engine - an 8-cylinder, inverted V type. It was planned to install one MG-17 machine gun.
Experienced Hs.121a flew for the first time on January 4, 1934. under the direction of Professor Schuebel. The plane turned out to be very unstable, and the reaction to the rudders was slow. The pilot gave negative feedback on all handling positions. It was obvious that the Hs.121 would not arouse the interest of the commissariat, but Nikolaus and his designer, despite being very busy with other work, were not going to admit defeat with the first project - work began almost immediately on reworking the second of the three ordered aircraft already in the form of a low-wing . The new aircraft was ready in three months under the designation Hs.125a. Attempts to bring the Hs.121a to fruition were unsuccessful, and the testing of the aircraft was never completed.
Crew |
1 |
Dimensions |
Wing span, m |
10.00 |
Wing area, m² |
14.00 |
Height, m |
1.85 |
Length, m |
7.30 |
Powerplant |
1 × PE Argus As-10C, power hp |
1 × 240 |
Weights, kg: |
Empty weight |
710 |
Gross weight |
960 |
Performance |
Maximum speed, km/h |
275 |
Cruise speed, km/h |
245 |
Service ceiling, m |
6,500 |
Service range, m |
500 |
Maximum rate of climb, m/min |
500 |
Armament |
1 × 7.9 mm MG-17 machine gun with cartridges per barrel:
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500 |
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Drawingа Hs 121а
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