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Siemens-Schuckert Forssman

The Siemens-Schuckert Forssman was a prototype bomber aircraft designed and built in Germany in 1914 and 1915.[5][6][7] When its performance proved inadequate for its intended role, even after numerous modifications, the German Inspectorate of Flying Troops (the Idflieg) eventually accepted it into service as a trainer.[3][4] Shortly after its acceptance into military service, the aircraft's fuselage fractured while on the ground, ending its career.[4]

Forssman
Role Bomber
National origin Germany
Manufacturer Siemens-Schuckert
Designer Villehad Forssman[1][2]
First flight Spring 1915[1]
Primary user Luftstreitkräfte[3][4]
Number built 1[4][5][6]

The aircraft is sometimes known as the Siemens-Schuckert Forssman R,[8] the "R" alluding to the designation that the Idflieg assigned to multi-engine aircraft in late 1915.[9] However, the Forssman did not meet all the criteria of the "R" designation — for example, its engines were not serviceable in flight — and the "R" designation only came into use after the Forssman was built.[10] If the Forssman received any military designation at all, that designation is not now known.[10]

Design and development

The Forssman was a large, four-engined, three-bay biplane with an extensively glazed, fully enclosed cabin.[7] The wings were unstaggered and of uneven span,[11] and the undercarriage consisted of two mainwheels carried on a common axle, plus a tailskid.[11] The tail was of conventional layout with a single fin.[7] Power was supplied by 110 hp (82 kW) Mercedes D.III engines mounted on short struts on the lower mainplane.[1][7] The design bore such a strong resemblance to the contemporary Sikorsky Ilya Muromets bombers produced in Russia that Jane's Encyclopedia of Aviation describes it as "virtually a copy" of that aircraft,[6] and in their book on German multi-engine types of World War I, Haddow and Grosz comment that designer Villehad Forssman "was content to copy the Sikorsky configuration almost line-for-line".[12]

Construction commenced in October 1914, and was completed by spring 1915.[1][7] Early test flights, probably limited to short hops, revealed multiple shortcomings in the design.[7] As originally completed, the wings were braced between the second and third cell by only a single strut.[7] Reinforcements to the wings added a second strut aft of this position, together with a set of diagonal struts to support the overhang of the upper wings[7] Other modifications at this time included rigging the wings with a slight dihedral to improve lateral stability,[7] adding a second tailfin and rudder to improve control,[7] and grafting an open gun position onto the front of the fuselage to improve the aircraft's centre of gravity.[1][7]

Even with these modifications in place, the Forssman could not fulfil the Idflieg's acceptance criteria, and Villehad Forssman severed his connections with Siemens-Schuckert owing to the failure of his design.[13] With Siemens-Schuckert still eager to recoup its investment in the design, the firm assigned Harald Wolff to improve the aircraft. Wolff deleted the tacked-on pulpit from the nose and redesigned the forward fuselage to taper to a sharp point, surmounted by a teardrop-shaped cupola for the pilot.[13] The redesign also replaced the two inner D.III engines with more powerful Mercedes D.IVa engines mounted on faired struts.[13] The outer engines remained unchanged, but were moved from their original position to mountings on faired struts midway in the interplane gap, to improve propeller efficiency.[13] Gun positions were added in the nose and in dorsal and ventral locations in the fuselage, although all these positions remained faired-over during testing and there is no evidence that armament was ever fitted.[13] In September 1915, and after another pilot had refused to fly the aircraft following some ground tests, Lt Walter Höndorf agreed to test the redesigned Forssman.[13] After a one or two hops, the aircraft turned over on its nose while alighting.[13] The nose was crushed, and the leading-edge spar in the upper wing was fractured.[13]

Despite all setbacks, Siemens-Schuckert still wanted to sell the aircraft, and commenced another rebuild.[13] The nose was redesigned again, into a rounded, blunt configuration with a gun position atop.[13] The pilot's position was relocated either behind the nose windows or to an open cockpit on top of the fuselage.[13] By now, the aircraft had acquired the nickname Ladenhüter (literally, "shelf warmer" or, idiomatically, "white elephant") and pilots refused to fly it.[13] Siemens-Schuckert director Walter Reichel negotiated a price discount for the Idflieg if they would accept the aircraft to a lower specification.[14] The Idflieg accepted, and reduced the acceptance criteria to the aircraft reaching 2,000 m (6,562 ft) in 30 minutes while carrying a useful load of 1,000 kg (2,205 lb) and enough fuel for an endurance of 4 hours.[15] Reichel now offered Bruno and Franz Steffen ten percent of the sale price if they could perform an acceptance flight to meet the Idflieg's requirements. The Steffen brothers examined the Forssman and Bruno agreed to make the flight, against the recommendations of friends and associates.[16] Franz's calculations based on the construction drawings showed the aircraft safe to fly, although the fuselage to be structurally weak immediately aft of the wings.[16]

After a successful 300-metre (984 ft) hop,[17] Bruno Steffen planned to fly the Forssman on its acceptance flight with four passengers aboard, as he had for his own R.I design.[4] However, everyone whom he invited declined, including the members of the Idflieg acceptance committee, and so he made the flight alone.[4] Carrying the required 1,000-kilogram payload, Steffen reached 2,000 metres in 28 minutes, and then climbed another 100 metres (328 ft) before returning to the ground.[4] While descending, one engine failed, followed shortly by the other three.[4] Nevertheless, Steffen made a safe landing and the acceptance criteria were verified.[4]

Although now obsolescent,[3] the Idflieg accepted the Forssman into service in April 1916 as a trainer.[3][4] Further development of the design was halted, although the aircraft's ballast was moved to counter tail heaviness that Steffen encountered on the acceptance flight.[4] Shortly after acceptance, the aircraft's fuselage fractured just aft of the wings, due to engine vibrations while running the engines on the ground.[4] The Forssman was dismantled at that point,[4] and Bruno Steffen expressed relief at the news, as the aircraft would not be able to endanger other lives.[10]

Specifications (as modified in late 1915)

Data from Gray & Thetford 1962, p.571

General characteristics

  • Crew: 4+
  • Length: 16.5 m (54 ft 1.75 in)
  • Wingspan: 24 m (78 ft 9 in)
  • Wing area: 140 m2 (1,512 sq ft)
  • Empty weight: 4,000 kg (8,800 lb)
  • Gross weight: 5,200 kg (11,400 lb)
  • Powerplant: 2 × Mercedes D.III , 82 kW (110 hp) each
  • Powerplant: 2 × Mercedes D.IVa , 164 kW (220 hp) each

Performance

  • Maximum speed: 120 km/h (75 mph, 65 kn)
  • Maximum glide ratio: 38.5
  • Rate of climb: 1.15 m/s (226 ft/min)

Notes

  1. ^ a b c d e Grey & Thetford 1962, p.570
  2. ^ Haddow & Grosz 1963, p.163
  3. ^ a b c d Grey & Thetford 1962, p.571
  4. ^ a b c d e f g h i j k l m Haddow & Grosz 1963, p.170
  5. ^ a b Grey & Thetford 1962, p.570–71
  6. ^ a b c Taylor 1989, p.808
  7. ^ a b c d e f g h i j k Haddow & Grosz 1963, p.164
  8. ^ for example, by Haddow & Grosz, and by the Royal Air Force Museum Aircraft Thesaurus
  9. ^ Haddow & Grosz 1963, p.1
  10. ^ a b c Haddow & Grosz 1963, p.172
  11. ^ a b Haddow & Grosz 1963, p.165
  12. ^ Haddow & Grosz 1963, p.162
  13. ^ a b c d e f g h i j k l Haddow & Grosz 1963, p.166
  14. ^ Haddow & Grosz 1963, p.167
  15. ^ Haddow & Grosz 1963, p.167–68
  16. ^ a b Haddow & Grosz 1963, p.168
  17. ^ Haddow & Grosz 1963, p.169

References

  • Gray, Peter; Owen Thetford (1962). German Aircraft of the First World War. London: Putnam.
  • Haddow, G.W.; Peter M. Grosz (1962). The German Giants: The Story of the R-planes 1914–1919. London: Putnam.
  • Sollinger, Günther (2009). Villehad Forssman: Constructing German Bombers 1914–1918. Moscow: Rusavia.
  • Taylor, Michael J.H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
  • Ward, Kevin (2002). . Royal Air Force Museum Aircraft Thesaurus. London: Collections Trust. Archived from the original on 2011-07-26. Retrieved 2011-04-25.

siemens, schuckert, forssman, prototype, bomber, aircraft, designed, built, germany, 1914, 1915, when, performance, proved, inadequate, intended, role, even, after, numerous, modifications, german, inspectorate, flying, troops, idflieg, eventually, accepted, i. The Siemens Schuckert Forssman was a prototype bomber aircraft designed and built in Germany in 1914 and 1915 5 6 7 When its performance proved inadequate for its intended role even after numerous modifications the German Inspectorate of Flying Troops the Idflieg eventually accepted it into service as a trainer 3 4 Shortly after its acceptance into military service the aircraft s fuselage fractured while on the ground ending its career 4 ForssmanRole BomberNational origin GermanyManufacturer Siemens SchuckertDesigner Villehad Forssman 1 2 First flight Spring 1915 1 Primary user Luftstreitkrafte 3 4 Number built 1 4 5 6 The aircraft is sometimes known as the Siemens Schuckert Forssman R 8 the R alluding to the designation that the Idflieg assigned to multi engine aircraft in late 1915 9 However the Forssman did not meet all the criteria of the R designation for example its engines were not serviceable in flight and the R designation only came into use after the Forssman was built 10 If the Forssman received any military designation at all that designation is not now known 10 Contents 1 Design and development 2 Specifications as modified in late 1915 3 Notes 4 ReferencesDesign and development EditThe Forssman was a large four engined three bay biplane with an extensively glazed fully enclosed cabin 7 The wings were unstaggered and of uneven span 11 and the undercarriage consisted of two mainwheels carried on a common axle plus a tailskid 11 The tail was of conventional layout with a single fin 7 Power was supplied by 110 hp 82 kW Mercedes D III engines mounted on short struts on the lower mainplane 1 7 The design bore such a strong resemblance to the contemporary Sikorsky Ilya Muromets bombers produced in Russia that Jane s Encyclopedia of Aviation describes it as virtually a copy of that aircraft 6 and in their book on German multi engine types of World War I Haddow and Grosz comment that designer Villehad Forssman was content to copy the Sikorsky configuration almost line for line 12 Construction commenced in October 1914 and was completed by spring 1915 1 7 Early test flights probably limited to short hops revealed multiple shortcomings in the design 7 As originally completed the wings were braced between the second and third cell by only a single strut 7 Reinforcements to the wings added a second strut aft of this position together with a set of diagonal struts to support the overhang of the upper wings 7 Other modifications at this time included rigging the wings with a slight dihedral to improve lateral stability 7 adding a second tailfin and rudder to improve control 7 and grafting an open gun position onto the front of the fuselage to improve the aircraft s centre of gravity 1 7 Even with these modifications in place the Forssman could not fulfil the Idflieg s acceptance criteria and Villehad Forssman severed his connections with Siemens Schuckert owing to the failure of his design 13 With Siemens Schuckert still eager to recoup its investment in the design the firm assigned Harald Wolff to improve the aircraft Wolff deleted the tacked on pulpit from the nose and redesigned the forward fuselage to taper to a sharp point surmounted by a teardrop shaped cupola for the pilot 13 The redesign also replaced the two inner D III engines with more powerful Mercedes D IVa engines mounted on faired struts 13 The outer engines remained unchanged but were moved from their original position to mountings on faired struts midway in the interplane gap to improve propeller efficiency 13 Gun positions were added in the nose and in dorsal and ventral locations in the fuselage although all these positions remained faired over during testing and there is no evidence that armament was ever fitted 13 In September 1915 and after another pilot had refused to fly the aircraft following some ground tests Lt Walter Hondorf agreed to test the redesigned Forssman 13 After a one or two hops the aircraft turned over on its nose while alighting 13 The nose was crushed and the leading edge spar in the upper wing was fractured 13 Despite all setbacks Siemens Schuckert still wanted to sell the aircraft and commenced another rebuild 13 The nose was redesigned again into a rounded blunt configuration with a gun position atop 13 The pilot s position was relocated either behind the nose windows or to an open cockpit on top of the fuselage 13 By now the aircraft had acquired the nickname Ladenhuter literally shelf warmer or idiomatically white elephant and pilots refused to fly it 13 Siemens Schuckert director Walter Reichel negotiated a price discount for the Idflieg if they would accept the aircraft to a lower specification 14 The Idflieg accepted and reduced the acceptance criteria to the aircraft reaching 2 000 m 6 562 ft in 30 minutes while carrying a useful load of 1 000 kg 2 205 lb and enough fuel for an endurance of 4 hours 15 Reichel now offered Bruno and Franz Steffen ten percent of the sale price if they could perform an acceptance flight to meet the Idflieg s requirements The Steffen brothers examined the Forssman and Bruno agreed to make the flight against the recommendations of friends and associates 16 Franz s calculations based on the construction drawings showed the aircraft safe to fly although the fuselage to be structurally weak immediately aft of the wings 16 After a successful 300 metre 984 ft hop 17 Bruno Steffen planned to fly the Forssman on its acceptance flight with four passengers aboard as he had for his own R I design 4 However everyone whom he invited declined including the members of the Idflieg acceptance committee and so he made the flight alone 4 Carrying the required 1 000 kilogram payload Steffen reached 2 000 metres in 28 minutes and then climbed another 100 metres 328 ft before returning to the ground 4 While descending one engine failed followed shortly by the other three 4 Nevertheless Steffen made a safe landing and the acceptance criteria were verified 4 Although now obsolescent 3 the Idflieg accepted the Forssman into service in April 1916 as a trainer 3 4 Further development of the design was halted although the aircraft s ballast was moved to counter tail heaviness that Steffen encountered on the acceptance flight 4 Shortly after acceptance the aircraft s fuselage fractured just aft of the wings due to engine vibrations while running the engines on the ground 4 The Forssman was dismantled at that point 4 and Bruno Steffen expressed relief at the news as the aircraft would not be able to endanger other lives 10 Specifications as modified in late 1915 EditData from Gray amp Thetford 1962 p 571General characteristicsCrew 4 Length 16 5 m 54 ft 1 75 in Wingspan 24 m 78 ft 9 in Wing area 140 m2 1 512 sq ft Empty weight 4 000 kg 8 800 lb Gross weight 5 200 kg 11 400 lb Powerplant 2 Mercedes D III 82 kW 110 hp each Powerplant 2 Mercedes D IVa 164 kW 220 hp eachPerformance Maximum speed 120 km h 75 mph 65 kn Maximum glide ratio 38 5 Rate of climb 1 15 m s 226 ft min Notes Edit a b c d e Grey amp Thetford 1962 p 570 Haddow amp Grosz 1963 p 163 a b c d Grey amp Thetford 1962 p 571 a b c d e f g h i j k l m Haddow amp Grosz 1963 p 170 a b Grey amp Thetford 1962 p 570 71 a b c Taylor 1989 p 808 a b c d e f g h i j k Haddow amp Grosz 1963 p 164 for example by Haddow amp Grosz and by the Royal Air Force Museum Aircraft Thesaurus Haddow amp Grosz 1963 p 1 a b c Haddow amp Grosz 1963 p 172 a b Haddow amp Grosz 1963 p 165 Haddow amp Grosz 1963 p 162 a b c d e f g h i j k l Haddow amp Grosz 1963 p 166 Haddow amp Grosz 1963 p 167 Haddow amp Grosz 1963 p 167 68 a b Haddow amp Grosz 1963 p 168 Haddow amp Grosz 1963 p 169References Edit Wikimedia Commons has media related to Siemens Schuckert Forsmann R Gray Peter Owen Thetford 1962 German Aircraft of the First World War London Putnam Haddow G W Peter M Grosz 1962 The German Giants The Story of the R planes 1914 1919 London Putnam Sollinger Gunther 2009 Villehad Forssman Constructing German Bombers 1914 1918 Moscow Rusavia Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions Ward Kevin 2002 Siemens Schuckert Royal Air Force Museum Aircraft Thesaurus London Collections Trust Archived from the original on 2011 07 26 Retrieved 2011 04 25 Retrieved from https en wikipedia org w index php title Siemens Schuckert Forssman amp oldid 1046901878, wikipedia, wiki, book, books, library,

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