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Curtiss F9C Sparrowhawk

The Curtiss F9C Sparrowhawk is a light 1930s biplane fighter aircraft that was carried by the United States Navy airships USS Akron and Macon.

It is an example of a parasite fighter, a small airplane designed to be deployed from a larger aircraft such as an airship or bomber.

On 20 August 1929, off New Jersey, a Vought UO-1 biplane hooked to the bottom of the Navy airship USS Los Angeles for a second time in the US and was carried by the larger craft.

After matching its speed to that of the dirigible, the biplane flew close underneath the Los Angeles.

A large hook mounted above the top wing of the biplane was caught by a U-shaped yoke mounted below the Los Angeles, which then carried the biplane for 3 or 4 minutes.

The pilot of the biplane pulled a cord which released the hook from the yoke, and he then flew clear of the dirigible and landed normally.

Although designed as a pursuit plane or fighter, the Sparrowhawk’s primary duty in service was reconnaissance, enabling the airships it served to search a much wider area of ocean.

The Sparrowhawk was primarily chosen for service aboard the large rigid-framed airships Akron and Macon because of its small size (20.2 ft (6.2 m) long and with only a 25.5 ft (7.8 m) wingspan), though its weight, handling and range characteristics, and also downward visibility from the cockpit, were not ideal for its reconnaissance role.

The theoretical maximum capacity of the airships’ hangar was five aircraft, one in each hangar bay and one stored on the trapeze but, in the Akron, two structural girders obstructed the aft two hangar bays, limiting her to a maximum complement of three Sparrowhawks.

A modification to remove this limitation was pending at the time of the airship’s loss. 

Macon had no such limitation and she routinely carried four airplanes.

To achieve launching and recovery from the airship in flight, a ‘skyhook’ system was developed.

The Sparrowhawk had a hook mounted above its top wing that attached to the crossbar of a trapeze mounted on the carrier airship.

For launching, the biplane’s hook was engaged on the trapeze inside the airship’s (internal) hangar, the trapeze was lowered clear of the hull into the (moving) airship’s slipstream and, engine running, the Sparrowhawk would then disengage its hook and fall away from the airship.

For recovery, the biplane would fly underneath its mother ship, until beneath the trapeze, climb up from below, and hook onto the crossbar.

The width of the trapeze crossbar allowed a certain lateral leeway in approach, the biplane’s hook mounting had a guide rail to provide protection for the turning propeller, and engagement of the hook was automatic on positive contact between hook and trapeze.

More than one attempt might have to be made before a successful engagement was achieved, for example in gusty conditions.

Once the Sparrowhawk was securely caught, it could then be hoisted by the trapeze back within the airship’s hull, the engine being cut as it passed the hangar door.

Although seemingly a tricky manoeuvre, pilots soon learned the technique and it was described as being much easier than landing on a moving, pitching and rolling aircraft carrier. 

Almost inevitably, the pilots soon acquired the epithet “The men on the Flying Trapeze” and their aircraft were decorated with appropriate unit emblems.

Once the system was fully developed, in order to increase their scouting endurance while the airship was on over-water operations, the Sparrowhawks would have their landing gear removed and replaced by a fuel tank.

When the airship was returning to base, the biplanes’ landing gear would be replaced so that they could land independently again.

For much of their service with the airships, the Sparrowhawk’s effectiveness was greatly hampered by their poor radio equipment, and they were effectively limited to remaining within sight of the airship.

However, in 1934 new direction-finding sets and new voice radios were fitted which allowed operations beyond visual range, exploiting the extended range offered by the belly fuel tanks and allowing the more vulnerable mother ship to stay clear of trouble.

One interesting use of the Sparrowhawks was to act as ‘flying ballast’.

The airship could take off with additional ballast or fuel aboard instead of its airplanes.

Once the airship was cruising, the aircraft would be flown aboard, the additional weight being supported by dynamic lift until the airship lightened.

Variants

XF9C-1

First prototype, one built, Scrapped in 1936.

XF9C-2

Second prototype, One built. 

F9C-2 Sparrowhawk

Single-seat fighter biplane, 6 built. 

Specifications

F9C-2

Crew

1

Length

20 ft 2.0 in (6.147 m)

Wingspan

25 ft 6.0 in (7.772 m)

Height

10 ft 6 in (3.2 m)

Wing area

172.79 sq ft (16.053 m2)

Airfoil

Clark YH

Empty weight

2,089 lb (948 kg)

Gross weight

2,776 lb (1,259 kg)

Powerplant

1 × Wright R-975-E3 9-cyl air-cooled radial piston engine,

438 hp (327 kW)

Performance

Maximum speed

176.5 mph (284.0 km/h, 153.4 kn)

Range

297 mi (478 km, 258 nmi)

Service ceiling

19,200 ft (5,900 m)

Rate of climb

1,700 ft/min (8.6 m/s)

Wing loading

16 lb/sq ft (78 kg/m2)

Power/mass

0.086 hp/lb (0.259 kW/kg)

Armament

Guns

2 × .30 in (7.62 mm) Browning machine guns.

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