Apollo Ultralight Aircraft Apollo Fox

Fixed Wing Single Engine

Aircraft Information

ICAO Code
AFOX
Manufacturer
Apollo Ultralight Aircraft
Model
Apollo Fox
Aircraft Type
Fixed Wing Single Engine
Primary Role
General Aviation

Technical Data

Engine Type
Inline
Engine Model
582/912UL/912ULS
Production Years
1998-present
Units Produced
More than 50
First Flight
1998
Notable Operators
Private owners, Flight training schools

The Apollo Fox is a Hungarian-built ultralight aircraft that brought modern STOL capabilities and innovative folding wing technology to the light sport aviation market. First flown in 1998, it is a strut-braced high-wing monoplane with side-by-side seating for two in an enclosed cockpit, powered by Rotax engines ranging from 65 to 100 horsepower. With a 30-foot wingspan that folds in just 10 minutes and a maximum takeoff weight of 450 kilograms, the aircraft demonstrated exceptional reliability during a remarkable 25,000-kilometer flight from Hungary to Australia. The Apollo Fox is manufactured by Apollo Ultralight Aircraft in Eger, Hungary.

Design Heritage and Development

The Apollo Fox emerged from a distinguished lineage of successful homebuilt aircraft designs. Apollo Ultralight Aircraft adapted their design from the Aeropro Eurofox, which itself was a metric conversion of the proven American Denney Kitfox. This design heritage traces back to the Avid Flyer, connecting the Apollo Fox to decades of refined short takeoff and landing aircraft development.

Engineers at Apollo Ultralight Aircraft specifically adapted the design to meet both Fédération Aéronautique Internationale microlight regulations and United States light-sport aircraft certification requirements. The aircraft also conforms to British BCAR Section S standards, demonstrating the manufacturer's commitment to international market compatibility. By 2003, just five years after first flight, Apollo had delivered more than 50 aircraft to customers across multiple countries.

Innovative Engineering Solutions

The Apollo Fox incorporates several distinctive engineering features that set it apart in the ultralight market. The aircraft's most notable innovation is its wing folding system, which allows a single person to fold the 30-foot wingspan in exactly 10 minutes for hangar storage or road transport. This capability transforms the aircraft from a flying machine into a towable package, dramatically reducing storage costs for owners.

The structural design combines proven materials and construction techniques. Apollo builds the fuselage from welded chrome molybdenum steel tubing, providing exceptional strength while maintaining light weight. Ceconite fabric covers both fuselage and wings, offering weather resistance and ease of maintenance. The wing structure features two aluminum spars supported by 14 main ribs and 13 auxiliary ribs, creating a robust framework capable of handling the stresses of short-field operations.

Junkers-style flaperons provide both aileron and flap functions, enhancing low-speed control authority essential for STOL performance. V-struts and jury struts support the high-wing configuration, distributing flight loads efficiently while maintaining the aircraft's distinctive appearance.

Power and Performance Options

Apollo offers the Fox with three primary engine configurations to meet varying performance and budget requirements. The entry-level Rotax 582 produces 65 horsepower from its two-cylinder, liquid-cooled design, providing adequate performance for training and recreational flying. The four-cylinder Rotax 912UL delivers 80 horsepower with improved reliability and fuel efficiency from its four-stroke design. At the top of the range, the Rotax 912ULS generates 100 horsepower, offering the best climb performance and payload capacity.

With the most powerful engine option, the Apollo Fox achieves a weight-to-power ratio of 5.625 kilograms per horsepower, providing sprightly performance despite its utilitarian mission. The aircraft carries 62 liters of fuel in wing-mounted tanks, ensuring adequate range for cross-country flights. Propeller options include traditional wooden two-blade units or modern ground-adjustable pitch three- or four-blade designs constructed from glass fiber or carbon fiber.

Record-Setting Achievement

In 2003, the Apollo Fox achieved international recognition when Hungarian pilots Andor Kántás and Csongor Lathky flew a Rotax 912ULS-powered example from Sármellék, Hungary, to Sydney, Australia. This extraordinary journey covered approximately 25,000 kilometers without any ground support team, relying entirely on the aircraft's reliability and the pilots' skill.

Remarkably, the two pilots reported zero technical problems during the entire transcontinental flight, providing compelling evidence of the aircraft's mechanical dependability. This achievement demonstrated that properly designed and maintained ultralight aircraft could accomplish missions previously reserved for much larger and more expensive aircraft.

Manufacturing and Certification

Apollo Ultralight Aircraft operates from Eger, Hungary, where the company manufactures not only the Apollo Fox but an entire range of ultralight aircraft. The company's product line includes five ultralight trike models designated Delta Jet, Jet Star, Monsoon, Racer GT, and C15D Toples, plus the Classic fixed-wing microlight and the Gyro AG1 gyroplane.

The Apollo Fox holds type certification in Belgium, Sweden, Hungary, France, Croatia, Romania, and Norway, reflecting Apollo's systematic approach to international market development. This multi-country certification process requires meeting diverse regulatory standards and demonstrates the aircraft's fundamental airworthiness across varying operational environments.

Contemporary Operations

Production continues into the present decade, with aircraft still rolling off Apollo's Hungarian production line as recently as 2022. A Norwegian-registered example from that production year confirms the model's ongoing market viability and manufacturer support.

The Apollo Fox serves primarily in recreational and personal transportation roles, where its STOL capabilities and folding wing convenience provide distinct advantages over conventional aircraft. Bush flying operations particularly benefit from the aircraft's short-field performance, while the wing folding feature appeals to pilots facing expensive hangar costs or limited storage facilities. The 110-centimeter cabin width provides comfortable side-by-side seating, making the aircraft suitable for flight training and recreational flying with passengers.