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Aviation History
1961
1961 - 1725.PDF
FLIGHT, 23 November 1961 831 (£•; Iliffe Transport Publications Ltd 1961 •sions: Span, 158ft 9in; length. 136ft 5in; height empty, 47ft;a, 2,466 sq ft; sweepback at quarter-chord, 7.05 .Dimensions: wing area, 0 it; sweepnacic i quariur-tiiuiu, I.«J •Weights: Max take-off. 300.0001b; max landing, 250,0001b; zero fuel. 730 0001b; design capacity payload. 100.0001b; weight less fuel, crewand pay load, 129,6001b. Payload accommodation: Cabin volume. 6.100 cu ft on upper deckfor passengers or freight. 5,400 cu ft on lower deck for freight; 900 cu ft for passengers' baggage; cabin accommodational length, 79ft; maxinternal width, 16ft 3in; max height. 13ft 5in; max usable floor area (less flight deck), 948 sq ft on upper deck for passengers. 840 sq ft onlower deck for freight; dimensions of largest door, 12ft > 12ft. the whole of the cross-section being available on opening the swing-nose;max number of seats (both decks). 255 at 32in pitch. Fuel capacity: 12.000 Imp gal.Water-methanol capacity: 320 Imp gal. Performance: Opt-cost (i.e.. typical) cruising speed at 17.5OOU (SK)and 230 0001b, 341kt; at 27.500ft (LR) and 230.0001b. 316kt; corres sfc 0 0435 n.m./lb (SR). 0.057 n.m./lb (LR); take-off field length,balanced field, max weight, ISA, SL. 9.600ft; landing field length, scheduled distance, max landing weight. ISA. SL, 5.400ft; range A(max pavload), 3,200 n.m.; range B (max fuel), 5,000 n.m.; corres payload,"69.0001b; cruise Mach number, 0.635; VNE. 320kt IAS; VNO,260kt IAS; Vso. 107kt IAS. SIPA Societe lndustrielle Pour V Aeronautique. 178 Avenue de Neuilly, Neuilly-sur-Seine. Sipa Presence S-272 The Presence was first presented at the ParisSalon in May 1961. It is a twin-Astazou light transport freighter and executive project, to which market reaction is now being assessed. An unusual feature is the provision of a swing-nose.Powerplant: Two Turbomeca Astazou II turboprops of 562 e.h.p. each driving Ratier FH 76 7ft 2in propellers.Dimensions: Span. 57ft lin; length. 45ft 7in; height empty, 15tt lin; wing area, 355 sq ft.Weights: Max take-off. 10,7361b; max landing. 10.2511b; zero fuel, 8,0911b; capacity payload. 3.5301b; weight less fuel, crew and payload.6,6141b (transport), 6,3821b (cargo). Pavtoad accommodation: Cabin volume (less flight deck), 635 cu tt;baggage and freight volume. 56 cu ft; cabin accommodational length. 21ft• max internal width, 7ft; max height, 5ft 6in; max usable floorarea (less flight deck), 129 sq ft; dimensions of largest door, 51m - 53in; max number of seats, 12 (or 16 side-by-side) at 35in pitch. Fuel capacity: 396 US gal.Water-methanol capacity: 10.5 US gal. Performance: Opt-cost (i.e., typical) cruising speed at 20,000tt ana10,7361b, 224kt; corres s.f.c, O.5371b/h.p./hr; take-off field length. 1 755ft; landinu field lenath. 1.720ft; range A (max payload). 162 n.m.; range B (max fuel), 1.350 n.m.; corres payload, 1,0801b; cruise Mach number. 0.36; VNO. 224kt IAS; Vso. 61.5kt IAS. SUD-AVIATION Societe Nationale de Constructions Aeromiutii/iws, 37 Boulevard de Montmorency, Paris. S.E.2010 Armagnac The biggest and heaviest piston-engined airliner to see regular service, the Armagnac first flew on April 2. 1949. Eight production aircraft were built in 1950-53. but none is now operational. Powerplant: Four Pratt & Whitney R-4360-B1 3 of 3.500 b.h.p.. driving Curtiss propellers. Data appeared in Flight. November 20. 1959. page 614. S O.30P Bretagne Derived from the S.O.30N (Gnome Rhone N48 49) which first flew on February 26, 1945. and from the S.O.30R Bellatrix (Gnome Rhone 14.Rs). the Bretagne went into production toan Air France specification. Fifty were built up to 1954 and delivered to Aiele Azur. Air Algerie. Air Maroc. Cosara. and to the French Services.The Bretagne is now operated only by the latter for military and VIP transport Two versions were built, the 30P-1 and the 3OP-2 with 2,400h.p. Pratt & Whitney R-28OO-CA 18s. _ _ . Powerplanv Two Pratt & Whitney R-2800-43 driving Curtiss Electric 13ft 5in propellers. Data appeared in Flight for November 20. 1959, page 615. S.E.161 Languedoc A development of the Bloch 160 and of the Bloch161 the Languedoc was put into production with Gnome Rhones in 1945, the first flying on September 17 of that year. Some 55 were built France's bid for supersonic supremacy: the Super Caravelle, in the de- velopment of which the British Aircraft Corporation may co-operate
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