Pope Thunderbird P-2

{{Infobox aircraft begin

| name=Pope Thunderbird P-2

| image=

| caption=

}}{{Infobox aircraft type

| type=Homebuilt aircraft

| national origin=United States

| manufacturer=

| designer=Leon Pope

| first flight=

| introduced=

| retired=

| status=

| primary user=

| more users=

| produced=

| number built=

| program cost=

| unit cost=

| developed from=

| variants with their own articles=

}}

The Pope Thunderbird is an American homebuilt biplane designed by Leon Pope.

Design and development

The Pope Thunderbird P-2 is a single engine, conventional landing gear-equipped, open cockpit biplane.{{cite magazine|magazine=Flying|date=November 1960|title=Experimental Aircraft Fly-In |pages=36–37|volume=67|issue=5}}{{cite magazine|last=Kohn|first=Leo J|magazine=Flying|date=December 1961|pages=34–35|title=EAA Fly-in|volume=69|issue=6}} The aircraft was designed by Leon Pope of Plymouth, Michigan and made its maiden flight on June 18, 1959.

Specifications

{{Aircraft specs

|ref=Jane's All The World's Aircraft 1961–62Taylor 1961, p. 309.

|prime units?=imp

|genhide=

|crew=1

|capacity=

|length m=

|length ft=15

|length in=0

|length note=

|span m=

|span ft=18

|span in=3

|span note=

|upper span m=

|upper span ft=

|upper span in=

|upper span note=

|lower span m=

|lower span ft=

|lower span in=

|lower span note=

|height ft=5

|height in=9

|wing area sqft=120

|aspect ratio=5.7:1

|airfoil=S-1A

|empty weight kg=

|empty weight lb=800

|empty weight note=

|gross weight kg=

|gross weight lb=1080

|gross weight note=

|fuel capacity=

|more general=

|eng1 number=1

|eng1 name=Lycoming O-235-C

|eng1 type=four-cylinder horizontally opposed piston aircraft engine

|eng1 kw=

|eng1 hp=100

|prop blade number=

|prop name=

|prop dia m=

|prop dia ft=

|prop dia in=

|prop dia note=

|perfhide=

|max speed kmh=

|max speed mph=135|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=115

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=55

|stall speed kts=

|stall speed note=

|never exceed speed kmh=

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

|range km=

|range miles=

|range nmi=

|range note=3{{frac|1|2}} h

|endurance=

|ceiling m=

|ceiling ft=

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=1000

|climb rate note=

|time to altitude=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=

|wing loading note=

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=

|thrust/weight=

|more performance=

|avionics=

}}

References

{{reflist}}

  • {{cite book|last=Taylor |first=John W. R. |authorlink= John W. R. Taylor |title=Jane's All The World's Aircraft 1961–62 |year=1961 |publisher= Sampson Low, Marston & Company, Ltd. |location=London}}

Category:Homebuilt aircraft