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MAIN INDEX > PROTOTYPES/EXPERIMENTAL >
Henschel Hs 130


Henschel Hs 130.

Type:
  Hs 128: High-Altitude research
  Hs 130A & E: Reconaissance
  Hs 130B & C: Bomber
Origin: Henschel Flugzeugwerke AG
  Models:
  Hs 128 V1 and V2
  Hs 130A through F
First Flight:
  Hs 130V1: 1939
  Hs 130E: Sept. 1942


Powerplant:
V1: Daimler-Benz DB 600 with DVL turbochargers
   Number: Two     Horsepower: 1,175hp

V2: Jumo 210 with two-stage turbochargers
   Number: Two     Horsepower: N/A

C: DB 603
   Number: Two     Horsepower: 1,850hp

E: DB 603B supercharged by DB 605T in the fuselage.
   Number: Two     Horsepower: 1,860hp

F: BMW 801TJ
   Number: Four     Horsepower: 1,800hp

Dimensions:
Wing span:
    Hs 130V1: 85 ft. 4½ in.)
    Hs 130A-0: 29.00m (95 ft. 1¾ in.)
    Hs 130E-0: 33.00m (108 ft. 3¼ in.)
Wing Surface Area: N/A
Length:
    Hs 130A-0: 14.95m (49 ft. ½ in.)
    Hs 130E-0: 22.00m (72 ft. 2 in.)
Height:
    Hs 130A-0: 4.90m (16 ft. 1 in.)
    Hs 130E-0: 5.60m (18 ft. 4½ in.)
  Weights:
Empty:
    Hs 130A-0: N/A
    Hs 130E-0: 12,200kg (26,900 lb.)
Loaded:
    Hs 130A-0: 11,680kg (25,750 lb.)
    Hs 130E-0: 18,100kg (39,900 lb.)

Performance:
Maximum Speed:
    Hs 130A-0: 292 mph (470 kph)
    Hs 130E-0: 379 mph (610 kph)
Range:
    Hs 130A-0: 1,385 miles (2230km)
    Hs 130E-0: 1,860 miles (3000km)


Armament: C-Bomber
Two Twin MG 131 barbettes
One MG 15 in tail

Bomb Load: C-Bomber
8,816 lb (4000kg) of bombs in internal bay


Development of the Hs 130 began with two Hs 128 prototypes, which first flew on 11 April 1939, with the second prototype flying on 20 February 1940. Both prototypes were research aircraft, used for testing pressurized cabins, engine superchargers, and cantilever wings. Different engines powered the two prototypes; the V1 by Daimler-Benz DB 601s and the V2 by Junkers Jumo 210s. Both had fixed landing gear. While trials of the two prototypes were not successful, the potential of a high altitude aircraft caught the attention of Theodor Rowehl, commander of the Luftwaffe's special reconnaissance unit. Rowehl's interest in the Hs 128's potential for high-altitude reconnaissance missions led Reich Air Ministry to instruct Henschel to continue development of the Hs 128 as a reconnaissance aircraft under the designation Hs 130A.

Three prototype aircraft Hs 130 As were built, the first flying on 23 May 1940. Five pre-production Hs 130A-0's followed, being delivered in early 1941, and featured DB 601R engines, a single-stage supercharger, retractable landing gear, and a bay in the rear to house two Rb75/30 cameras for reconnaissance. The five Hs 130A-0s subsequently underwent trials and testing, which revealed significant problems with the aircraft performance, and reliability problems which prevented operational use. Two further modified Hs 130A-0s was produced under the designation Hs 130A-0/U6 and featured a greater wingspan, DB 605B engines, Hirth superchargers, GM-1 nitrous oxide power boosting, and under-wing drop tanks, and being ready for flight testing in November 1943, demonstrating an absolute ceiling of 15,500 m (50,570 ft). The Hs 130A-0/U6 variant as well as the other Hs 130A-0s proved unsatisfactory and were never flown operationally.


Henschel Hs 130.

Further development of the Hs 130 led to bomber variants. The planned Hs 130B was almost the same as the Hs 130A, but with a bomb bay in place of the camera bay, but was never built. The Hs 130C was built as a competitor for the "Bomber B" project, and was very different from the Hs 130A, featuring a shorter wing span, remotely-controlled defensive armament, a more extensively glazed (but still pressurized) cabin and up to 4,000 kg (8,800 lb) of bombs. Three prototypes, V1, V2, and V3 were built, with V1 and V2 were powered by BMW 801 radials, and V3, featuring full armament by DB 603A engines. Further development of the Hs 130 as a reconnaissance aircraft continued with the Hs 130D, which was planned to have DB 605 engines and a complex two-stage supercharger, but was again unbuilt.

The Hs 130E was a re-working of the Hs 130A with the Höhen Zentrale (HZ)-Anlage system in place of conventional superchargers. HZ-Anlage installed a third engine in the fuselage, a DB 605, the only purpose of which was to power a large supercharger to supply air to the wing-mounted DB 603B engines. Such a system had first been tried some twenty-five years previously, on the R.30/16 example of the Zeppelin-Staaken R.VI bomber. Another difference from the Hs 130A was the nose, which was extended forward to offset the weight of the HZ-Anlage engine in the fuselage. Also underwing fuel tanks could be fitted to provide fuel for three engines, and air scoops were fitted under the fuselage to supply the fuselage engine.

Three prototype Hs 130Es were built; Hs 130E V1 first flew in September 1942, and could reach 12,500 m (41,010 ft) when HZ-Anlage was employed. Hs 130E V2 was lost due to an engine fire; V3 was built to replace it. An order for seven pre-production Hs 130E-0s followed, first flying in May 1943, together with a production order was placed for 100 Hs 130E-1s which were to have a remotely controlled defensive armament and provisions for underwing bombs. The order was cancelled due to continuing problems suffered by the Hs 130E-0's HZ-Anlange system. An Hs 130F was planned, which was hoped to solve the problems with HZ-Anlage, by using four supercharged BMW 801 engines, but was never built.


Sources:
Gunston, Bill & Wood, Tony - Hitler's Luftwaffe, 1977, Salamander Books Ltd., London
Wikipedia - Henschel Hs 130

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