Min speed: 35 kt 40 mph 64 kmh
Cruise speed: 81 kt 93 mph 150 kmh
Vne: 97 kt 112 mph 180 kmh


Take off distance over 50ft (15m) obstacle: 460 ft | 140 m
Landing distance over 50ft (15m) obstacle: 660 ft | 200 m

Max. take off weight: 450 kg | 992 lbs
Empty weight: 274 kg | 604 lbs

Engine: Rotax 582, 912, Jabiru 2200

Other aircraft information:
Photo from: www.ul-bolaget.se

Text from: http://www.halley.hu/

The Apollo Fox is built according to the "BCAR? Section S constuction norm.

The aircraft has welded steel alloy tube fuselage covered with ?ceconite? fabric. The wing are made of aluminium alloy both spars and ribs and then covered with ceconite.

Wing can be folded backwards. One pilote can do it within 10 minits. The landing gears are aluminium plate sheet as year suspension. Wheels are equipped with hidraulic disc or mechanical drum brakes. Apollo Fox has very good rudder harmony and very easy to fly and land.

Available tail or nose wheel configurations.

Engine: Rotax 582 UL Mod 99 (65Hp), 912UL (80 Hp), 912 ULS (100 Hp), Jabiru 2200 (80Hp), Subaru EA 81 (100 Hp).


Halley Apollo Fox

High wing single piston ultralight.

This page lists the major suppliers to the Halley Apollo Fox aircraft program.


Manufacturer
Halley Kft

Power Systems / Engines
BRP-Rotax GmbH & Co. KG Piston Engines: 582, 912 or 912S engines
Halley Kft Piston Engines: Converted Subaru car engine
HKS Aviation Co. Ltd. Piston Engines: HKS 700 engine
Jabiru Aircraft Pty Ltd. Piston Engines: 2200 engine
ULPower Piston Engines: UL260i engine