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Henschel Hs 121

From Wikipedia, the free encyclopedia
1934 German advanced trainer aircraft
Henschel Hs 121
General information
TypeAdvanced trainer
National originGermany
ManufacturerHenscel Flugzeug-Werke A.G.
Designer
Erich Koch
Number built1
History
First flight4 January 1934

TheHenschel Hs 121 was the first aircraft built by the German Henschel company. It was a high-wingmonoplane with an inline engine, fixed undercarriage and single, open cockpit, designed as an advancedtrainer. Only one aircraft was produced, in 1933–4, as a testpiece for the Air Ministry.

Development

[edit]

Henschel & Son ofKassel were originally known as manufacturers of locomotives, though they later produced lorries and buses. In 1933 they set up an aviation subsidiary based atSchönefeld with a branch atJohannisthal.[1] New aircraft manufacturers who intended to produce aircraft for theLuftwaffe 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, withgull 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 andtailplane 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.[1]

Power was from a 180 kW (240 hp) Argus As 10C inverted in-line engine.[1]

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. Only one Hs 121 was built.

Specifications

[edit]
Henschel Hs 121 3-view drawing from L'Aerophile September 1939

Data fromGrey 1972, p. 157c

General characteristics

  • Crew: 1
  • Length: 7.3 m (23 ft 11.5 in)
  • Wingspan: 10.0 m (32 ft 10 in)
  • Height: 2.8 m (9 ft 2 in)
  • Wing area: 14.0 m2 (150 sq ft)
  • Empty weight: 760 kg (1,672 lb)
  • Gross weight: 960 kg (2,112 lb)
  • Powerplant: 1 ×Argus As 10C eight-cylinder inverted air-cooled in-line , 180 kW (240 hp)

Performance

  • Maximum speed: 278 km/h (173 mph, 150 kn)
  • Cruise speed: 250 km/h (155 mph, 135 kn)
  • Endurance: 2 hours
  • Service ceiling: 6,500 m (21,320 ft)
  • Rate of climb: 8.3 m/s (1,640 ft/min) to 2,000 m (6,560 ft)

References

[edit]
Wikimedia Commons has media related toHenschel Hs 121.
Citation
  1. ^abcGrey 1972, p. 157c
Cited sources
  • Grey, C.G. (1972).Jane's All the World's Aircraft 1938. London: David & Charles.ISBN 0-7153-5734-4.
Henschel aircraft and missiles
1 to 100
101 to 200
201 to 300
301 to 349
Post-349 (non-sequential)
  • 1 Not assigned
  • 2 Unofficial/proposed
  • 3 Assigned, but not used before RLM was dissolved
  • 4 Assigned to captured aircraft
  • 5 Unconfirmed
  • 6 Propaganda/cover designation
  • 7 Assigned to multiple types

Note: Official RLM designations had the prefix "8-", but this was usually dropped and replaced with the manufacturer's prefix.

Authority control databasesEdit this at Wikidata
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