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==Specifications==
==Specifications==
{{Aircraft specs
{{aerospecs
|ref=<!-- reference -->"Pitcairn, A G A, Pitcairn-Cierva, Pitcairn-Larsen"
|ref=<!-- reference -->"Pitcairn, A G A, Pitcairn-Cierva, Pitcairn-Larsen"
|prime units? = imp
|met or eng?=<!-- eng for US/UK aircraft, met for all others. You MUST include one or the other here, or no specifications will show -->eng

|crew=One pilot
|crew=One pilot
|capacity=1 passenger
|capacity=1 passenger
Line 43: Line 42:
|span ft=22
|span ft=22
|span in=9
|span in=9
|swept m=<!-- swing-wings -->
|swept ft=<!-- swing-wings -->
|swept in=<!-- swing-wings -->
|rot number=<!-- helicopters -->1
|rot number=<!-- helicopters -->1
|rot dia m=<!-- helicopters -->11.28
|rot dia m=<!-- helicopters -->11.28
|rot dia ft=<!-- helicopters -->37
|rot dia ft=<!-- helicopters -->37
|rot dia in=<!-- helicopters -->0
|rot dia in=<!-- helicopters -->0
|dia m=<!-- airships etc -->
|dia ft=<!-- airships etc -->
|dia in=<!-- airships etc -->
|width m=<!-- if applicable -->
|width ft=<!-- if applicable -->
|width in=<!-- if applicable -->
|height m=
|height ft=
|height in=
|wing area sqm=
|wing area sqft=
|swept area sqm=<!-- swing-wings -->
|swept area sqft=<!-- swing-wings -->
|rot area sqm=<!-- helicopters -->99.9
|rot area sqm=<!-- helicopters -->99.9
|rot area sqft=<!-- helicopters -->10.75
|rot area sqft=<!-- helicopters -->10.75
|volume m3=<!-- lighter-than-air -->
|volume ft3=<!-- lighter-than-air -->
|aspect ratio=<!-- sailplanes -->
|wing profile=<!-- sailplanes -->
|empty weight kg=
|empty weight lb=
|gross weight kg=
|gross weight lb=
|lift kg=<!-- lighter-than-air -->
|lift lb=<!-- lighter-than-air -->

|eng1 number=1
|eng1 number=1
|eng1 type=[[Kinner B-5]]
|eng1 name=[[Kinner B-5]]
|eng1 kw=<!-- prop engines -->93
|eng1 kw=<!-- prop engines -->93
|eng1 hp=<!-- prop engines -->125
|eng1 hp=<!-- prop engines -->125
|eng1 kn=<!-- jet/rocket engines -->
|eng1 lbf=<!-- jet/rocket engines -->
|eng1 kn-ab=<!-- afterburners -->
|eng1 lbf-ab=<!-- afterburners -->
|eng2 number=
|eng2 type=
|eng2 kw=<!-- prop engines -->
|eng2 hp=<!-- prop engines -->
|eng2 kn=<!-- jet/rocket engines -->
|eng2 lbf=<!-- jet/rocket engines -->
|eng2 kn-ab=<!-- afterburners -->
|eng2 lbf-ab=<!-- afterburners -->

|max speed kmh=140
|max speed kmh=140
|max speed mph=90
|max speed mph=90
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=<!-- if max speed unknown -->
|cruise speed mph=<!-- if max speed unknown -->
|stall speed kmh=<!-- aerobatic and STOL aircraft -->
|stall speed mph=<!-- aerobatic and STOL aircraft -->
|range km=400
|range km=400
|range miles=250
|range miles=250
|endurance h=<!-- if range unknown -->
|endurance min=<!-- if range unknown -->
|ceiling m=3,000
|ceiling m=3,000
|ceiling ft=10,000
|ceiling ft=10,000
|g limits=<!-- aerobatic aircraft -->
|roll rate=<!-- aerobatic aircraft -->
|glide ratio=<!-- sailplanes -->
|climb rate ms=
|climb rate ftmin=
|sink rate ms=<!-- sailplanes -->
|sink rate ftmin=<!-- sailplanes -->

|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}
}}
<!-- ==See also== -->
<!-- ==See also== -->

Revision as of 20:53, 26 July 2020

PAA-1
This Pitcairn PAA-1 autogiro was flown at Langley for the NACA investigation of an experimental cantilevered three-bladed rotor. June 1943.
Role Sport autogyro
National origin United States
Manufacturer Pitcairn-Cierva Autogiro Company
First flight 1931
Number built 25

The Pitcairn PAA-1 was an autogyro developed in the United States in the early 1930s.[1] Of similar configuration to Pitcairn's earlier machines, the PAA-1 had an airplane-like fuselage with two open cockpits in tandem and a tractor-mounted engine in the nose.[2] It was also equipped with small wings, which carried control surfaces, rather than using the rotor for flight control.[2] It was a smaller and lighter machine than its predecessors and was designed specifically with private pilots in mind.[1][2]

Variants

  • PAA-1 - main production version with Kinner B-5 engine[2]
  • PA-20 - improved version with Kinner R-5 engine[2]
  • PA-24 - version with twin tails and Kinner R-5 engine, modified from existing PAA-1s and PA-20s[2]


Specifications

Data from "Pitcairn, A G A, Pitcairn-Cierva, Pitcairn-Larsen"

General characteristics

  • Crew: One pilot
  • Capacity: 1 passenger
  • Length: 18 ft 7 in (5.66 m)
  • Wingspan: 22 ft 9 in (6.93 m)
  • Powerplant: 1 × Kinner B-5 , 125 hp (93 kW)
  • Main rotor diameter: 37 ft 0 in (11.28 m)
  • Main rotor area: 10.75 sq ft (99.9 m2)

Performance

  • Maximum speed: 90 mph (140 km/h, 78 kn)
  • Range: 250 mi (400 km, 220 nmi)
  • Service ceiling: 10,000 ft (3,000 m)

References

Notes
  1. ^ a b Taylor 1989, p.734
  2. ^ a b c d e f The Illustrated Encyclopedia of Aircraft, p.2739
Bibliography
  • The Illustrated Encyclopedia of Aircraft. London: Aerospace Publishing.
  • "Pitcairn, A G A, Pitcairn-Cierva, Pitcairn-Larsen". Aerofiles. Retrieved 2009-01-15.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.

External links

Wikimedia Commons has media related to Pitcairn PAA-1.
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