Pitcairn PAA-1: Difference between revisions
Content deleted Content added
No edit summary |
Citation bot (talk | contribs) Misc citation tidying. | Use this bot. Report bugs. | Suggested by AManWithNoPlan | #UCB_CommandLine |
||
(10 intermediate revisions by 10 users not shown) | |||
Line 1: | Line 1: | ||
__NOTOC__ |
|||
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
||
{|{{Infobox |
{|{{Infobox aircraft begin |
||
| name=PAA-1 |
| name=PAA-1 |
||
| image=Pitcairn PAA-1 at Langley's NACA Research Center, 1943.jpg |
|||
| image= |
|||
| caption=This Pitcairn PAA-1 autogiro was flown at Langley for the NACA investigation of an experimental cantilevered three-bladed rotor. June 1943. |
|||
| caption= |
|||
}}{{Infobox |
}}{{Infobox aircraft type |
||
| type=Sport autogyro |
| type=Sport autogyro |
||
| national origin=United States |
| national origin=United States |
||
Line 22: | Line 21: | ||
The '''Pitcairn PAA-1''' was an autogyro developed in the United States in the early 1930s.<ref name="JEA">Taylor 1989, p.734</ref> 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.<ref name="IEA">''The Illustrated Encyclopedia of Aircraft'', p.2739</ref> It was also equipped with small wings, which carried control surfaces, rather than using the rotor for flight control.<ref name="IEA"/> It was a smaller and lighter machine than its predecessors and was designed specifically with private pilots in mind.<ref name="JEA"/><ref name="IEA"/> |
The '''Pitcairn PAA-1''' was an autogyro developed in the United States in the early 1930s.<ref name="JEA">Taylor 1989, p.734</ref> 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.<ref name="IEA">''The Illustrated Encyclopedia of Aircraft'', p.2739</ref> It was also equipped with small wings, which carried control surfaces, rather than using the rotor for flight control.<ref name="IEA"/> It was a smaller and lighter machine than its predecessors and was designed specifically with private pilots in mind.<ref name="JEA"/><ref name="IEA"/> |
||
<!-- ==Development== --> |
<!-- ==Development== --> |
||
<!-- ==Operational history== --> |
<!-- ==Operational history== --> |
||
Line 34: | Line 32: | ||
==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 46: | Line 43: | ||
|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 |
|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== --> |
||
Line 135: | Line 71: | ||
==References== |
==References== |
||
;Notes |
;Notes |
||
⚫ | |||
{{reflist}} |
{{reflist}} |
||
;Bibliography |
;Bibliography |
||
* {{cite book |title=The Illustrated Encyclopedia of Aircraft |publisher=Aerospace Publishing|location=London |
* {{cite book |title=The Illustrated Encyclopedia of Aircraft |publisher=Aerospace Publishing|location=London }} |
||
* {{cite web| title=Pitcairn, A G A, Pitcairn-Cierva, Pitcairn-Larsen |work=Aerofiles |url=http://www.aerofiles.com/_pitc.html | |
* {{cite web| title=Pitcairn, A G A, Pitcairn-Cierva, Pitcairn-Larsen |work=Aerofiles |url=http://www.aerofiles.com/_pitc.html |access-date=2009-01-15}} |
||
* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |
* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London }} |
||
==External links== |
==External links== |
||
⚫ | |||
* [https://books.google.com/books?id=9ycDAAAAMBAJ |
* [https://books.google.com/books?id=9ycDAAAAMBAJ&dq=Popular+Science+motor+gun+boat&pg=PA28 "Will Autogiro Banish Present Plane?", March 1931, pg 28] |
||
{{Pitcairn aircraft}} |
{{Pitcairn aircraft}} |
||
[[Category:United States sport aircraft |
[[Category:1930s United States sport aircraft]] |
||
[[Category:Pitcairn aircraft|PAA-1]] |
[[Category:Pitcairn aircraft|PAA-1]] |
||
[[Category: |
[[Category:Single-engined tractor autogyros]] |
Latest revision as of 17:15, 17 March 2023
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[edit]
- 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[edit]
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[edit]
- Notes
- 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[edit]
Wikimedia Commons has media related to Pitcairn PAA-1.