Thaden T-2

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{{Infobox Aircraft Begin

| name=Thaden T-2

| image=Thaden T-2 left front Aero Digest August 1929.jpg

| caption=

}}{{Infobox Aircraft Type

| type=Cabin monoplane

| national origin=United States

| manufacturer=Thaden Metal Aircraft Company

| designer=Herbert von Thaden

| first flight=1928

| introduced=

| retired=

| status=

| primary user=

| number built=1

| developed from=

| variants with their own articles=

}}

The Thaden T-2 was a 1920s American four-seat all-metal cabin monoplane built by the Thaden Metal Aircraft Company of San Francisco, California, USA.

Design and development

The Thaden Metal Aircraft Company was formed by Herbert von Thaden, a former United States Army Signal Corps pilot and engineer, to work on developing the first American all-metal aircraft. Following on from the strut-braced T-1 the T-2 was a smaller four-seat high-wing cantilever monoplane with flaps, powered by a {{convert|150|hp|kW|0|abbr=on}} Comet radial engine.

Specifications

File:Thaden_T-2_3-view_Aero_Digest_August_1929.png

{{Aircraft specs

|ref=Aero Digest August 1929

|prime units?=imp

|genhide=

|crew=one

|capacity=two or three passengers

|length ft=24

|length in=11

|length note=

|span ft=39

|span in=

|span note=

|height ft=7

|height in=9

|height note=

|wing area sqft=225

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=

|empty weight lb=

|empty weight note=

|gross weight kg=

|gross weight lb=

|gross weight note=

|max takeoff weight kg=

|max takeoff weight lb=

|max takeoff weight note=

|fuel capacity={{cvt|50|USgal|Impgal l}}

|more general=

|eng1 number=1

|eng1 name=Comet 7-D

|eng1 type=7 cylinder radial engine

|eng1 hp=150

|eng1 note=at 1,800 rpm

|power original=

|more power=

|prop blade number=2

|prop name=Westinghouse Micarta

|prop dia m=

|prop dia ft=

|prop dia in=

|prop dia note=

|perfhide=

|max speed mph=121

|max speed note=

|cruise speed mph=100

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=

|stall speed kts=

|stall speed note=

|range km=

|range miles=

|range nmi=

|range note=

|endurance=

|ceiling ft=14000

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ftmin=800

|climb rate note=

|time to altitude=

|sink rate ms=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=

|wing loading note=

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=

|more performance=

  • Landing speed, flaps down: {{cvt|46|mph|km/h}}

}}

See also

{{Portal|Aviation}}

References

{{commons category|Thaden T-2}}

{{reflist|refs=

Orbis 1985, p. 3000

{{cite magazine |editor=Horsefall, J.E.|title=American Eagle Phaeton biplane|journal=Aero Digest|date= August 1929 |page=134,136 |url=https://archive.org/details/aerodigest1415unse/page/122/mode/2up| publisher=Aeronautical Digest Publishing Corp| location=New York City}}>

}}

;Bibliography

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{{Thaden aircraft}}

Category:1920s United States civil utility aircraft

Category:Economy of San Francisco

Category:Single-engined tractor aircraft

Category:High-wing aircraft

Category:Aircraft first flown in 1928

{{aero-1920s-stub}}