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词条 Rigault RP.01B
释义

  1. Development

  2. Operational history

  3. Specifications (RP.01B)

  4. References

  5. External links

name=Rigault RP.01B image=Rigault RP.01 F-WABO Mitry 29.05.57 edited-1.jpg caption=The RP.01B "Le Napalm" under construction at Mitry-Mory airfield near Paris in May 1957
}}{{Infobox Aircraft Type
type=light single-seat national origin=France manufacturer=Paul Rigault designer=Paul Rigault first flight=1958 introduced=1958 retired= status=No longer extant primary user=the builder number built=One developed from= variants with their own articles=
}}

The Rigault RP.01B was a French-built high-wing single-engined ultralight aircraft of the 1950s.

Development

The RP.01B was a one-off aircraft which was designed and built by Monsieur Paul Rigault at Mitry-Mory airfield to the NE of Paris.[1] The airfield now forms part of the site of Paris-Charles de Gaulle airport.

The aircraft was fitted with high-set wings which were supported by twin struts, a fixed tailwheel undercarriage and a single seat for the pilot owner. It was powered by a nine-cylinder Salmson 9 ADB air-cooled radial engine. It was of conventional wooden construction with plywood and fabric-covered fuselage and fabric-covered wings and control surfaces.[2]

Operational history

M. Rigault completed the aircraft during 1958 and named it "Le Napalm". He flew it regularly until at least early 1965.[3] The RP.01B is no longer extant.

Specifications (RP.01B)

{{aerospecs
|ref=Green, 1965
|met or eng?=eng
|crew=1
|capacity=
|length m=
|length ft=
|length in=
|span m=7.70
|span ft=25
|span in=3
|swept m=
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|rot number=
|rot dia m=
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|dia m=
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|width m=
|width ft=
|width in=
|height m=
|height ft=
|height in=
|wing area sqm=
|wing area sqft=
|swept area sqm=
|swept area sqft=
|rot area sqm=
|rot area sqft=
|volume m3=
|volume ft3=
|aspect ratio=
|wing profile=
|empty weight kg=
|empty weight lb=
|gross weight kg=324
|gross weight lb=714
|lift kg=
|lift lb=
|eng1 number=1
|eng1 type=Salmson 9 ADB
|eng1 kw=34
|eng1 hp=45
|eng1 kn=
|eng1 lbf=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 type=
|eng2 kw=
|eng2 hp=
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|eng2 kn-ab=
|eng2 lbf-ab=
|perfhide=Y
|max speed kmh=
|max speed mph=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|stall speed kmh=
|stall speed mph=
|range km=
|range miles=
|endurance h=
|endurance min=
|ceiling m=
|ceiling ft=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
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|sink rate ftmin=
}}

References

Notes
1. ^Butler, 1963, p. 113
2. ^Green, 1965, p. 62
3. ^Green, 1965, p. 62
Bibliography
{{refbegin}}
  • {{cite book|last=Butler|first=P.H.|title=French Civil Aircraft Register|year=1963|publisher=Merseyside Society of Aviation Enthusiasts|isbn=}}
  • {{cite book|last=Green|first=William|title=The Aircraft of the World|year=1965|publisher=MacDonald & Co. (Publishers) Ltd|isbn=}}
{{refend}}

External links

3 : French civil utility aircraft 1950–1959|High-wing aircraft|Aircraft first flown in 1958

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