Wikipedia

Sikorsky S-35

The Sikorsky S-35 was an American triple-engined sesquiplane transport later modified to use three-engines. It was designed and built by the Sikorsky Manufacturing Company for an attempt by René Fonck on a non-stop Atlantic crossing for the Orteig Prize. It was destroyed in the attempt.

S-35
Role Transatlantic sesquiplane
National origin United States
Manufacturer Sikorsky Manufacturing Company
First flight August 23, 1926
Number built 1

Design and development edit

The S-35 was designed as a twin-engined transport with a 1,000-mile (1,600-kilometre) range.[1] During 1926 René Fonck, a French First World War fighter ace, was looking for a multi-engine aircraft to enter a competition to be the first to fly non-stop from New York to Paris. Raymond Orteig offered a prize of $25,000.[1] Fonck had Sikorsky redesign the aircraft with three engines.[1]

The S-35 was a sesquiplane with a fixed tail-skid landing gear. It was modified to take three 425 hp (317 kW) Gnome-Rhône Jupiter 9A[a] radial engines and fitted with jettisonable auxiliary landing gear directly under the fuselage to support its weight at takeoff. Fuel was carried in tanks in the upper wing leading edge, the engine nacelles, and the fuselage. Fuel was pumped up to the wing tanks from which it fed the engines under gravity. The wing tanks alone gave four hours flight time.[2] As it was designed for passenger and transport use, the cabin behind the cockpit (described as "exceptionally large and roomy") was 4 ft (1.2 m) wide by 6 ft (1.8 m) high and 15 ft 6 in (4.72 m) long accessed by a door at the rear.[2]

These modifications took time to complete and the aircraft first flew on 23 August 1926 from Roosevelt Field.[1] Sikorsky started a series of test flights but as none were at the maximum takeoff weight of 24,200 lb (11,000 kg), Sikorsky wanted to delay the transatlantic crossing until early 1927, but the promoters of the flight would not accept a delay and the aircraft was prepared for the crossing.[1] Speaking after the accident to the French press, Fonck said that he had completed 27 hours test flying the S.35 at various weights including 280 passengers over the period.[3]

Operational history edit

The first transatlantic attempt was scheduled for the September 16 but was abandoned after the aircraft developed a fuel leak.[1] The next available break in the weather was to be the 21 September and the aircraft was fueled during the previous night from 50 barrels of gasoline. When the aircraft was weighed it was found to be 4,000 pounds (1,800 kg) overweight.[1] Fonck insisted on carrying a sofa and refrigerator on the journey.[citation needed] Fonck and his co-pilot Lt Lawrence Curtin of the U.S. Navy were joined by a radio operator and a Sikorsky mechanic for the flight.[1][b]

Departure was scheduled for sunrise and the takeoff began at 6:36.[5] In front of a large crowd at Roosevelt Field the aircraft gathered speed, the auxiliary landing gear broke away, the aircraft failed to get airborne and plunged down a steep slope at the end of the runway and burst into flames.[1][6] The two pilots escaped injury but the radio operator Charles Clavier and mechanic Jacob Islamoff were killed in the fire. The aircraft, which had cost $80,000, was not insured.[1]

Specifications (for Atlantic flight) edit

 
Sikorsky S-35 3-view drawing from Les Ailes, June 24, 1926

Data from Best[1]

General characteristics

  • Crew: four
  • Length: 44 ft 0 in (13.41 m)
  • Upper wingspan: 101 ft 0 in (30.78 m)
  • Lower wingspan: 76 ft 0 in (23.16 m)
  • Height: 16 ft 0 in (4.88 m)
  • Wing area: 1,095 sq ft (101.7 m2) [2]
  • Empty weight: 9,700 lb (4,400 kg) [c]
  • Gross weight: 20,000 lb (9,072 kg)
  • Max takeoff weight: 24,200 lb (11,000 kg)
  • Fuel capacity: 15,200 lb (6,900 kg) [2]
  • Powerplant: 3 × Gnome-Rhône Jupiter 9A radial engine, 425 hp (317 kW) each [d]
  • Propellers: 2-bladed, 10 ft 6 in (3.20 m) diameter

Performance

  • Maximum speed: 145 mph (233 km/h, 126 kn)
  • Endurance: 7 hours
  • Service ceiling: 16,800 ft (5,100 m)
  • Wing loading: 21.8[2] lb/sq ft (106 kg/m2)
  • Power/mass: 19 lb/hp[2]

See also edit

Aircraft of comparable role, configuration, and era

Notes edit

  1. ^ A license-built copy of a design by the aero-engine subsidiary of Bristol Aeroplane Company
  2. ^ Flight gave the originally announced crew accompanying Fonck as "Lieut. Allan Snody, U S. Navy (navigator), Capt. Homer Berry (second pilot), and Capt. John Irwin (wireless operator)"[4]
  3. ^ Flight gives 8,000 lb (3,600 kg) with a further 490 lb (220 kg) "equipment"[2]
  4. ^ Flight gives 400 hp (300 kW)[2]

References edit

  1. ^ a b c d e f g h i j k Best, Martin (2002). "Sikorsky American Fixed-Wing Aircraft, Part 1: Sikorsky S-29-A to S-35". Air-Britain Archive. 2002 (4): 127. ISSN 0262-4923.
  2. ^ a b c d e f g h Flight 30 September 1926 p640
  3. ^ "Capt. Fonck on his Accident". Flight. Vol. XIX, no. 13. 31 March 1927. p. 188.
  4. ^ "Capt. Fonck's Atlantic Flight". Flight. Vol. XVIII, no. 32. 1926-08-12. p. 491.
  5. ^ "New York- Paris Flight Tragedy". Flight. Vol. XVIII, no. 38. 23 September 1926. p. 628.
  6. ^ Joshua Stoff. Long Island aircraft crashes 1909-1959. p. 48.

Bibliography edit

  • Laureau, Patrick (February 2000). "La première tentative de traversée de l'Atlantique (1926): L'écheque du Sikorsky S-35" [The First Tentative Attempts to Cross the Atlantique: The Failure of the Sikorsky S-35]. Avions: Toute l'aéronautique et son histoire (in French) (83): 38–43. ISSN 1243-8650.
  • "The Sikorsky S.35". Flight. Vol. XVIII, no. 39. 30 September 1926. pp. 638–640 – via Internet Archive.

External links edit

 
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