Henschel Hs 132

Henschel's Hs 132 was a World War II dive bomber and interceptor aircraft of the German Luftwaffe that never saw service. The unorthodox design featured a top-mounted BMW 003 jet engine (identical in terms of make and position to the powerplant used by the Heinkel He 162) and the pilot in a prone position. The Soviet Army occupied the factory just as the Hs 132 V1 was nearing flight testing, the V2 and V3 being 80% and 75% completed.

Hs 132
An airbrushed drawing of the P.132
Role Dive bomber and Interceptor aircraft
Manufacturer Henschel Flugzeugwerke AG
Status Never flown
Primary user Luftwaffe
Produced 1945
Number built 4 prototypes

Design and development

There had been interest in the idea of a prone pilot for combat aircraft to reduce the effect of g-forces during maneuvering. Several aircraft had already experimented with this layout for various reasons, the Horten IIIf had a prone pilot, but this was primarily to reduce drag in this high-performance glider,[1] while the DFS 228 reconnaissance glider also used a prone pilot to make it easier to seal its pressurized cabin. It was not until the Berlin B9 was built specifically to test this arrangement for improved g-load that any serious effort toward development could be carried out.

Starting in early 1943, the Berlin B9 twin-piston engined experimental aircraft demonstrated that it was indeed possible for a pilot to fly the aircraft lying down, and that it did improve his ability to handle high loads. The pilot had an extremely restricted field of view upward or to the rear that made it suitable only for certain roles, including bombers or fighters or interceptors with a major speed advantage over their opposition.[2]

Based on this research, several late-war German designs followed the B9's lead and used a prone pilot. Better g-load performance was not the only reason, however, as this layout also reduced the frontal area of the aircraft. This was a serious concern for interceptors attacking the USAAF's B-17 Flying Fortress, as calculations showed that the chance of being hit by its defensive guns was largely a function of frontal area.

The genesis for the Hs 132 was an 18 February 1943 specification published by the German Air Ministry (RLM) calling for a single-seat shipping attack aircraft to counter an expected invasion of Europe. A piston-engined aircraft was called for at the time, but the performance requirements led to a switch to jet power.[2] Henschel submitted their design for RLM approval in April/May 1944, by which point they had already started wind tunnel testing the basic layout. The aircraft that emerged had a roughly cigar-shaped fuselage with short-span mid-set wings and a horizontal stabilizer with considerable dihedral ending in twin rounded-front vertical stabilizers.

The BMW 003 engine was mounted on the back of the aircraft above the wing, likely to make servicing easier due to the low ground height of the aircraft that put the engine roughly shoulder-height. The sharply dihedraled 'butterfly'-like twin rudder arrangement kept the tail surfaces clear of the jet efflux. The cockpit was completely faired into the fuselage contour, with a rounded clear nose-cone on the front of the aircraft. Behind this was the actual "window," a large armored-glass plate located some distance behind the extreme nose; the glazing extended almost to the wing root.[3] The design in terms of engine mounting and tailplane bore a very strong resemblance to the contemporary Volksjäger ("people's fighter") design competition winner, the Heinkel He 162 Spatz (sparrow). The basic A model carried one 500 kg (1,100 lb) bomb; it had no other armament. It was to begin its attack in a shallow dive outside the ships' range of fire, and after reaching a speed of 910 km/h (570 mph; 490 kn), the pilot would "toss" the bomb at the target using a simple computerized sight, and then climb back out of range. The aircraft was designed to withstand 12 g during pullout. The computerized bombsight was not delivered in time to be fitted to the aircraft.

Several other versions of the basic airframe were proposed as well. The Hs 132B used the Junkers Jumo 004 engine in place of the BMW 003, and added two 20 mm (0.79 in) MG 151/20 cannons. The HS 132C was a more extensively modified version intended for bomber interception, featuring the larger Heinkel HeS 011 engine, two 20 mm (0.79 in) 151/20s and two 30 mm (1.2 in) MK 103 or MK 108 cannons. The HeS 011, intended to power a wide variety of new and existing Luftwaffe aircraft (an example of the latter being the proposed D and P series of the Arado Ar 234 jet bomber), was still in the pre-production phase when the war ended. It was hoped that by the time the HS 132B became available, the Panzerblitz anti-tank missile would be in production and available for use. The Hs 132D included a new wing of increased span. A contract for six prototypes was approved in May 1944, and construction was begun in March 1945. Hs 132V1 was scheduled to have its first flight in June 1945, but the completed wings and fuselage were never mated, and Soviet forces captured the intact fuselage in May 1945 while the wings were never moved from their factory in France.

Variants
Hs 132A Dive bomber
BMW 003 turbojet engine, 1 × 500 kg (1,100 lb) bomb
Hs 132B Dive bomber/Anti-tank plane
Jumo 004 turbojet engine, 1 × 500 kg (1,102 lb) bomb, 2 × 20 mm MG 151 cannon, and/or six or eight Panzerblitz anti-tank rockets
Hs 132C Dive bomber
He S 011 turbojet engine, 1 × 500 kg (1,100 lb) bomb, 2 × 20 mm MG 151 cannon and 2 × 30 mm (1.2 in) MK 103 cannon
Hs 132D
Increased wingspan variant

Specifications (Hs 132A)

Data from German aircraft of the Second World War[4]

General characteristics

  • Crew: 1
  • Length: 8.9 m (29 ft 2 in)
  • Wingspan: 7.2 m (23 ft 7 in)
  • Wing area: 14.82 m2 (159.5 sq ft)
  • Gross weight: 3,400 kg (7,496 lb)
  • Powerplant: 1 × BMW 109-003E-2 turbojet engine, 7.8 kN (1,760 lbf) thrust
Hs 132B 1x 8.8 kN (1,980 lbf) Junkers Jumo 109-004B turbojet
Hs 132C 1x 12.75 kN (2,866 lbf) Heinkel-Hirth 109-011A turbojet

Performance

  • Maximum speed: 780 km/h (480 mph, 420 kn) without bomb at 6,000 m (20,000 ft) ; 700 km/h (430 mph; 380 kn) with bomb
  • Landing speed: 153 km/h (95 mph; 83 kn)
  • Range: 680 km (420 mi, 370 nmi) at 4,000 m (13,000 ft) ; 1,120 km (700 mi; 600 nmi) at 10,000 m (33,000 ft)
  • Service ceiling: 10,250 m (33,630 ft)

Armament

Hs 132A
1x 500 kg (1,100 lb) SD 500 bomb semi-resessed under the fuselage
Hs132B
2x nose mounted 20 mm (0.787 in) MG 151 cannon
1x 500 kg (1,100 lb) bomb semi-resessed under the fuselage
Hs 132C
2x nose mounted 20 mm (0.787 in) MG 151 cannon
2x nose mounted 30 mm (1.181 in) MK 103 cannon
or
2x nose mounted 20 mm (0.787 in) MG 151 cannon
1x 1,000 kg (2,200 lb) SC 1000 bomb semi-resessed under the fuselage
or
2x nose mounted 20 mm (0.787 in) MG 151 cannon
1x 1,000 kg (2,200 lb) PC 1000 RS Pol rocket-assisted armour-piercing bomb semi-resessed under the fuselage

See also

Aircraft of comparable role, configuration, and era

Related lists

References
Notes
  1. Horten H IIL, H IIIf, H IIIh, H VI V2 Archived 2008-01-11 at the Wayback Machine
  2. Berlin B9 Experimental Aircraft
  3. Christopher, John. The Race for Hitler's X-Planes (The Mill, Gloucestershire: History Press, 2013), p.147.
  4. Smith, J. Richard; Kay, Antony L. (1989). German aircraft of the Second World War. Nautical & Aviation Pub. Co. pp. 339–341. ISBN 978-0933852976.
Bibliography
  • Green, William. Warplanes of the Third Reich. London: Macdonald and Jane's Publishers Ltd., 1970 (fourth impression 1979). ISBN 0-356-02382-6.
  • Smith, J.Richard and Kay, Anthony. German Aircraft of the Second World War. London: Putnam & Company Ltd., 1972 (third impression 1978). ISBN 0-370-00024-2.
  • Wood, Tony and Gunston, Bill. Hitler's Luftwaffe: A pictorial history and technical encyclopedia of Hitler's air power in World War II. London: Salamander Books Ltd., 1977. ISBN 0-86101-005-1.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.