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词条 Swallow TP
释义

  1. Design and construction

  2. Variants

  3. Specifications (Swallow TP)

  4. References

  5. External links

name=Swallow TP image=Swallow TP at Yanks Chino 05.01.jpg caption=Swallow TP at Yanks Air Museum Chino California

}}{{Infobox Aircraft Type

type=Trainer national origin=United States manufacturer=Swallow designer=Amos O. Payne first flight=1928 introduced= retired= status= primary user= number built=~200 developed from= variants with their own articles=
}}

The Swallow TP was a trainer aircraft produced by the Swallow Airplane Company in the United States from 1928.

Design and construction

The TP was a simple and rugged biplane design with room for an instructor and student in tandem open cockpits. The fuselage was made from welded steel tubing, faired to shape and then fabric covered. The wings were typical of the day with Spruce spars, spruce & plywood ribs with fabric covering. Built to be easy to fly, and for ease of maintenance, the Swallow TP was quite popular with nearly 200 being built. Initially the TP was offered with the ubiquitous Curtiss OX-5. Later, it was offered with a choice of a Siemens-Halske, Kinner, or Warner engines. Most customers opted for the OX-5 which was the cheapest.[1]

Variants

Data from:Aerofiles[2]
TP

Main production variant with a Curtiss OX-5 engine, about 200 built.

TP-K

Production variant with a five-cylinder Kinner K-5 engine, 20 to 25 built.

TP-W

Production variant with a seven-cylinder Warner Scarab engine, three built

TP-Sh

Production variant with seven-cylinder Siemens-Halske Sh 14 engine.

Specifications (Swallow TP)

{{Aircraft specs
|ref=U.S. Civil Aircraft Vol.2[1]
|prime units?=imp


|crew=1
|capacity=1
|length ft=23
|length in=7
|span ft=30
|span in=11
|height ft=8
|height in=10
|wing area sqft=296
|aspect ratio=
|airfoil=
|empty weight lb=1283
|gross weight lb=1825
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Curtiss OX-5
|eng1 type=V-8 water-cooled piston engine
|eng1 hp=90
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|max speed mph=90
|cruise speed mph=75
|stall speed mph=33
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range miles=300
|range note=+
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=4724
|g limits=
|roll rate=
|climb rate ftmin=650
|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=
}}

References

1. ^{{cite book |last= Juptner |first= Joseph P. |title=U.S. Civil Aircraft Vol.2|year=1964 |publisher=Aero Publishers|location=Los Angeles |pages=20-21 }}
2. ^{{cite web |title=Swallow, New Swallow |work=Aerofiles.com|url=http://aerofiles.com/_swallow.html |accessdate=2008-10-21}}

External links

{{commons category|Swallow TP}}
  • FAA Approved Type Certificate 105 Swallow TP

1 : United States civil trainer aircraft 1920–1929

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