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词条 Sud-Ouest Bretagne
释义

  1. Design and devopment

  2. Operational history

  3. Variants

  4. Operators

     Military operators  Civil operators 

  5. Specifications (S.O.30P-2)

  6. See also

  7. References

  8. Further reading

name = S.O.30 Bretagneimage = SO.30P Bretagne No.40 Aeronavale Palas jets BLA 09.55.jpgcaption = SO.30P of the Aeronavale equipped with under-wing Palas auxiliary jets at Blackbushe Airport in 1955

}}{{Infobox Aircraft Type

type = Airliner and military transportmanufacturer = Sud-Ouestdesigner =first flight = 26 February 1945introduced =retired =produced =number built = 45status =unit cost =primary user = Air Francemore users = French Air Forcedeveloped from =variants with their own articles =
}}

The Sud-Ouest S.O.30 Bretagne was a 1940s French airliner built by Sud-Ouest.

Design and devopment

The Bretagne was designed by a group of designers and engineers who were based at Cannes from May 1941 following the invasion of France. The design was for a medium capacity civil transport, a twin-engined mid-wing cantilever all-metal monoplane. The prototype (designated the S.O.30N) first flew on 26 February 1945.

Operational history

The initial production version was designated the S.O.30P Bretagne with two versions with different engines. The aircraft operated with a crew of five and could carry between 30 and 43 passengers. A cargo version (the S.O.30C) with a revised interior and strengthened floor and large cargo door. The aircraft was operated as an airliner, but mainly by the French military forces as a medium transport.

Some aircraft were fitted with two underwing Turbomeca Palas turbojet engines for auxiliary power. Other aircraft were used for engine-trials fitted with the SNECMA Atar 101 and licence-built Rolls-Royce Nene turbojets.

Variants

S.O.30N
Tailwheel undercarriage prototype, c/n 01 built after the 1940 armistice and stored till after the war. The second S.O.30R c/n 02 was built in 1946 and later converted to the S.O.30 Nene, jet powered airliner test-bed.
S.O.30R Bellatrix
Two prototypes of the nosewheel undercarriage production model.
S.O.30C
cargo version, one built with belly loading hatches.
S.O.30P-1
production version with Pratt & Whitney R-2800-B43 engines.
S.O.30P-2
production version with Pratt & Whitney R-2800-CA13 engines.
S.O.30 Nene
One aircraft converted from S.O.30R c/n 02 for use as a testbed, powered by two Rolls-Royce Nenes.

Operators

Military operators

{{FRA}}
  • French Air Force[1]
  • French Navy[1]

Civil operators

{{ALG}}
  • Air Algérie[2]
{{FRA}}
  • Aigle Azur[1]
  • Air France[2]
  • COSARA based in French Indo-China[3]
{{IRN}}
  • Iranian Airways[2]
{{MAR}}
  • Air Maroc[2]

Specifications (S.O.30P-2)

{{Aircraft specs
|ref=Jane's All The World's Aircraft 1953–54[4], French postwar transport aircraft[5], [6]
|prime units?=met


|crew= 4
|passengers= 43
|length m=18.95
|span m=26.9
|height m=5.9
|wing area sqm=86.2
|aspect ratio=
|airfoil=
|empty weight kg=14000
|gross weight kg=
|max takeoff weight kg=20250
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=2
|eng1 name=Pratt & Whitney R-2800-CA18
|eng1 type=18-cyl. air-cooled radial piston engines
|eng1 hp=2434
|eng1 note=for take-off with water injection
|eng2 number=2
|eng2 name=Turbomeca Palas
|eng2 type=
|eng2 kN=
|eng2 note=optional {{convert|1.47|kN|lbf|abbr=on}} turbojet booster engines under the outer wings
|prop blade number=4
|prop name=constant-speed fully feathering propellers
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|max speed kmh=575
|cruise speed kmh=438
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=2175
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=8000
|g limits=
|roll rate=
|climb rate ms=6
|time to altitude=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|more performance=
|avionics=
}}

See also

{{aircontent
|related=
|similar aircraft=
  • Curtiss C-46 Commando
  • Vickers Valetta
  • Ilyushin Il-12

|sequence=
|lists=
  • List of military aircraft of France

|see also=
}}

References

{{commons category|Sud-Ouest Bretagne}}
Notes
1. ^Stroud 1966, p. 203.
2. ^Stroud 1966, p. 202.
3. ^Stroud 1966, pp. 202–203.
4. ^Bridgman 1953, pp. 152–153.
5. ^{{cite book|last1=Chillon|first1=J.|last2=Dubois|first2=J-P.|last3=Wegg|first3=J.|title=French postwar transport aircraft|date=1980|publisher=Air-Britain|location=Tonbridge|isbn=0851300782|pages=26-27}}
6. ^{{cite web|last1=Parmentier|first1=Bruno|title=S.N.C.A.S.O. SO-30P 'Bretagne' série 2|url=https://www.aviafrance.com/aviafrance1.php?ID=9658&ID_CONSTRUCTEUR=1145&ANNEE=0&ID_MISSION=0&MOTCLEF=|website=Aviafrance|accessdate=2 December 2017|language=French}}
Bibliography
{{refbegin}}
  • Bridgeman, Leonard. Jane's All The World's Aircraft 1953–54. London: Jane's All The World's Aircraft Publishing Company, 1953.
  • Stroud, John. European Transport Aircraft since 1910. London: Putnam, 1966.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). London: Orbis Publishing, 1985.
{{refend}}

Further reading

  • {{cite book |title=Jane's all the World's Aircraft 1947 |edition= |editor1-last=Bridgman |editor1-first=Leonard |year=1947 |publisher=Sampson Low, Marston & Co |location=London |pages=141c-142c}}
{{SNCASO aircraft}}

7 : French airliners 1940–1949|French military transport aircraft 1940–1949|Sud-Ouest aircraft|Mid-wing aircraft|Aircraft first flown in 1945|Twin-engined piston aircraft|Twin piston-engined tractor aircraft

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