Type Single seat advanced trainer
Engine 1 Argus As 10C
Dimensions Length 7,3 m, height 2,8 m, span 10,0 m, wing area 14,0 m2
Weights Empty 760 kg, flying weight 960 kg
Performance Max. speed 278 km/h, cruising speed 250 km/h, service ceiling 6500 m, climb 8,3 m/sec to 2000 m, endurance 2 h
Type Werk.Nr Registration History
V1 1 First flight 4/1 1934, crashed 30/1 1934.
V2 2 D-EOVA First flight 24/9 1934
Henschel & Son of Kassel were originally known as manufacturers of locomotives, though they later produced lorries and buses. In 1933 they set up an aviation subsidiary based at Schönefeld with a branch at Johannisthal. New aircraft manufacturers who intended to produce aircraft for the Luftwaffe had first to make a testpiece or masterpiece (Befahigungsnachweis) to prove their competence and the Hs 121 was Henschel's offering.

It was a high-wing braced monoplane, with gull wing roots to enhance the pilot's forward view from the open cockpit set well back behind the trailing edge. The wing was built around two metal spars with metal-covered leading edges and fabric elsewhere. There was solid bracing from near mid-wing to the lower fuselage and from this bracing inwards to the shoulder of the gull wing. The oval fuselage had a metal structure with metal covering. The tail was also a metal structure, with metal covering on the fin and tailplane but with fabric-covered control surfaces. There was wire bracing between fin and tailplane. The spatted main-wheels were carried on streamlined legs which angled outwards from the lower fuselage to increase the track.
It flew for the first time at Johannisthal on 4 January 1934. A test flight programme produced some modifications: the fin was braced, the tailplane extended and more bracing was added between the landing gear and the fuselage.