Boeing PW-9A

     
Název:
Name:
Boeing PW-9A Boeing PW-9A
Originální název:
Original Name:
Boeing PW-9A
Kategorie:
Category:
stíhací letoun fighter aeroplane
Výrobce:
Producer:
DD.MM.1926-DD.02.1927 Boeing Airplane Co., Seattle, Washington
Období výroby:
Production Period:
DD.MM.1926-DD.02.1927
Vyrobeno kusů:
Number of Produced:
23 (26-351-373)
První vzlet:
Maiden Flight:
DD.MM.1926
Osádka:
Crew:
1
Základní charakteristika:
Basic Characteristics:
 
Vzlet a přistání:
Take-off and Landing:
CTOL - konvenční vzlet a přistání CTOL - conventional take-off and landing
Uspořádání křídla:
Arrangement of Wing:
dvouplošník biplane
Uspořádání letounu:
Aircraft Concept:
klasické conventional
Podvozek:
Undercarriage:
pevný fixed
Přistávací zařízení:
Landing Gear:
kola wheels
Technické údaje:
Technical Data:
 
Hmotnost prázdného letounu:
Empty Weight:
878 kg 1936 lb
Vzletová hmotnost:
Take-off Weight:
1378 kg 3039 lb
Maximální vzletová hmotnost:
Maximum Take-off Weight:
? kg ? lb
Rozpětí:
Wingspan:
9.75 m 32ft
Délka:
Length:
7.14 m 23ft 5in
Výška:
Height:
2.49 m 8ft 2in
Plocha křídla:
Wing Area:
24.15 m2 260 ft2
Plošné zatížení:
Wing Loading:
? kg/m2 ? lb/ft2
Pohon:
Propulsion:
 
Kategorie:
Category:
pístový piston
Počet motorů:
Number of Engines:
1
Typ:
Type:
Curtiss D-12C o výkonu 324 kW
dvoulistá vrtule
Curtiss D-12C, power 435 hp
two-blade propeller
Objem palivových nádrží:
Fuel Tank Capacity:
235 l 62 US gal
Výkony:
Performance:
 
Maximální rychlost:
Maximum Speed:
262.3 km/h v 0 m 163 mph in 0 ft
Cestovní rychlost:
Cruise Speed:
228.5 km/h v ? m 142 mph in ? ft
Rychlost stoupání:
Climb Rate:
? m/s ? ft/min
Čas výstupu na výšku:
Time to Climb to:
? min do ? m ? min to ? ft
Operační dostup:
Service Ceiling:
6401 m 21000 ft
Dolet:
Range:
627.6 km 390 mi
Maximální dolet:
Maximum Range:
? km ? mi
Výzbroj:
Armament:
2x pevný synchronizovaný 7,62mm kulomet Browning nebo
1x 7,62mm a 1x 12,7mm kulomet Browning
2x fixed .30 Browning machine gun, or
1x fixed .30 and 1x .50 Browning machine gun
Uživatelské státy:
User States:
Poznámka:
Note:
- -
Zdroje:
Sources:
Bowers, Peter M. Boeing Aircraft since 1916. London, Putnam 1989. ISBN 0-85177-804-6.
United States Army and Air Force Fighters 1916-1961, Harleyford Publications, Letchworth 1961.
Pelletier, Alain. Boeing - The Complete Story. Haynes Publishing, Yeovil 2010. ISBN 978-1-84425-703-4.
www.americancombatplanes.com
http://joebaugher.com/usaf_fighters/pw9.html
http://www.aviastar.org/air/usa/boeing_pw-9.php
http://crimso.msk.ru/Site/Crafts/Craft30885.htm
URL : https://www.valka.cz/Boeing-PW-9A-t81677#299592 Version : 0
26. October 1925 was ordered 25 established , THE PW-9 under the designation PW-9A, the factory designation of Model 15A. The main difference represented the engine of the Curtiss D-12C (later renamed the V-1150-1), also had modified the wiring of the fuel, oil and cooling. From the outside they were from the previous version basically indistinguishable.The first machines were handed over 19. June 1926, the last 4. February of the following year.

The penultimate of the ordered machines, 26-374, was completed in the form of AT-3 (Boeing Model 68), an experimental advanced trainer aircraft with the engine of the Wright-Hispano Model E. The last PW-9A was then completed as the PW-9B (26-375) with the engine of the Curtiss D-12D (V-1150-3) engine. AT-3 was a failure, however, it was ordered 15 of the PW-9B. Even those were eventually built - the army has adjusted the specification and location PW-9B were built just slightly different to the PW-9C. PW-9B was adjusted to the standard PW-9A and handed over to the army in February 1927..
Boeing PW-9A - PW-9A, pravděpodobně 19. stíhací peruť, Havaj

PW-9A, pravděpodobně 19. stíhací peruť, Havaj
URL : https://www.valka.cz/Boeing-PW-9A-t81677#418150 Version : 0
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