Curtiss F11C Goshawk

Curtiss F11C Goshawk
Χώρα	Ηπα
Ρόλο	Carrier-borne Fighter & Fighter-Bomber
Πρώτη πτήση	September 1932
Ἀμή	30

Teh Κέρτις F11C Γκοσάουκ was a 1930s United States naval biplane fighter aircraft that saw limited success but was part of a long line of Curtiss Hawk airplanes built by the Curtiss Aeroplane and Motor Company for the American military.

Πηγή: RCurtiss F11C Goshawk στη Βικιπαίδεια

BFC-2 Walk Around
Φωτογράφος	Φώτιος Ρουτς
Εντοπισμού	Αγνοώ
Φωτογραφίες	22

BFC-2 01

BFC-2 02

BFC-2 03

BFC-2 04

BFC-2 05

BFC-2 07

BFC-2 06

BFC-2 08

BFC-2 09

Click on a photo and use the mouse scroll to view all photos

Wait, Searching Curtiss F11C Goshawk for you…

Δείτε επίσης:

Biplanes, Triplanes and Seaplanes
by Μάικλ Σαρπ
324 Pages · 2000

General Characteristics and Role

The Curtiss F11C Goshawk was a single-seat biplane fighter and dive bomber developed for the United States Navy in the early 1930s. It was the last in the line of Curtiss biplane fighters, evolved from the Curtiss Hawk family. Although initially designated as a fighter (F11C), its role quickly expanded, and the production version was re-designated as a two-seat fighter-bomber/scout (BFC-2). The Goshawk was a highly maneuverable aircraft, serving briefly as a primary fighter aboard US Navy aircraft carriers before being quickly superseded by the shift to monoplane designs in the mid-1930s.

Property	Typical Value (F11C-2 / BFC-2)
Ρόλο	Carrier-Based Fighter / Scout-Bomber
National Origin	Ηνωμένες Πολιτείες
Κατασκευαστής	Curtiss Αεροπλάνο και Εταιρεία Αυτοκινήτων
First Flight	March 1932
Πλήρωμα	1 (Pilot) or 2 (BFC-2/BF2C-1)
Μήκος	7.62 m (25 ft 0 in)
Εκπέτασμα	9.60 m (31 ft 6 in)
Ύψος	3.35 m (11 ft 0 in)
Empty Weight	1,217 kg (2,683 lb)
Gross Weight	1,739 kg (3,835 lb)

Powerplant and Performance

Engine: One Wright R-1820-78 Cyclone nine-cylinder, air-cooled radial engine.
Power Output: 522 kW (700 hp).
Maximum Speed: 331 km/h (206 mph; 179 kn) at 1,370 m (4,500 ft).
Cruise Speed: Approx. 257 km/h (160 mph; 140 kn).
Range: 868 km (539 mi; 469 nmi).
Service Ceiling: 7,830 m (25,700 ft).
Retractable Landing Gear: Later variants (like the BF2C-1) introduced a fully retractable undercarriage, a crucial step toward monoplane design adoption.

Armament and Variants

Fixed Armament: 2 x .30 in (7.62 mm) forward-firing Browning machine guns mounted above the engine cowling.
Bomb Load: 1 x 474 lb (215 kg) bomb carried under the fuselage.
- Dive Bomber Role: The aircraft was equipped with a trapeze mechanism under the fuselage that swung the bomb clear of the propeller arc during a vertical dive.
Major Variants:
- F11C-2: Initial fighter version.
- BFC-2: Redesignated production model focusing on the fighter-bomber/scout role.
- BF2C-1: Final variant with a fully retractable landing gear, quickly withdrawn due to structural failures caused by the new gear mechanism.
- Export: F11C-2s were sold to the Chinese Nationalist Air Force and the Turkish Air Force.