Hornet Microlights Invader 440 / Dual Striker

Hornet/Flexiform Sky Sails Invader 440/Dual Striker – A side by side two seat single engined flex wing aircraft with weight shift control. Rogallo wing with keel pocket. Pilot suspended below wing in trike unit, using bar to control pitch and yaw/rod by altering relative positions of trike unit and wing. Wing braced from above by kingpost and cables, from below by cables; bowsprit construction with 65% double surface; pre formed ribs. Undercarriage has three wheels in tricycle formation; steel spring suspension on nosewheel and rubber suspension on main wheels. Push right go left nose¬wheel steering independent from yaw control. Brakes on main wheels. Aluminium tube/ glass fibre trike unit, partially enplosed. Engine mounted below wing driving pusher propeller. All major components made from aircraft quality materials.
The Invader gives weather protection, quick rigging and ease of ground handling a high priority. The wind tunnel developed trike unit is almost fully enclosed, only the sides being open, and is of mono pole construction. The mono pole is an aerofoil rather than the usual round section and is mated to a one piece rear axle instead of the two piece plus tie wire arrangement commonly used with mono poles.
To cope with rough field operation, all three wheels have suspension and in addition the nose wheel geometry is arranged to give a self stabilising effect, so that the aircraft runs true even if the pilot makes a less than perfect touchdown. A hand operated brake is fitted to the main wheels, arranged so that it can be used as a parking brake. The fuel tank is made from aluminium alloy with internal baffles.
Rigging is confined to the wing and is hence claimed to take a maximum of 15 minutes. The trike unit has road tyres on the rear, running on stainless steel axles and taper=roller bearings, so that it can be towed complete on its own wheels. Wing fitment is the Flexiform Skysails Dual Striker, a fast wing which Hornet designer Richard Wolfenden says is well matched to the new trike unit.

Length overall 14.0 ft, 4.27 m.
Height overall 12.5 ft, 3.80m.
Wing span 38.0 ft, 11.58m.
Chord at root 9.0 ft, 2.74m.
Chord at tip 3.5ft, 1.07m.
Dihedral 2 degs.
Sweepback 15 degs.
Keel pocket depth 1.2ft, 0.37m.
Total wing area 250 sq.ft
23.2 sq.m.
Keel pocket area 3.5 sq.ft, 0.33 sq.m.
Wing aspect ratio 6.0/1.
Wheel track 4.3 ft, 1.31 m.
Nosewheel diameter overall 16 inch, 41 cm.
Main wheels diameter overall 16 inch, 41 cm.
Engine: Robin EC44, 50 hp.
Propeller diameter and pitch 60×34 inch, 1.52×0.86m.
Toothed belt reduction, ratio 2.8/1.
Max static thrust 280 lb, 127kg.
Power per unit area 0.20hp/sq.m, 2.2 hp/sq.m.
Fuel capacity 5.0 US gal, 4.2 Imp gal, 19.1 litre.
Empty weight 290 lb, 132kg.
Max take off weight 682 lb, 309kg.
Payload 392 lb, 1.78kg.
Max wing loading 2.73 lb/sq.m, 13.3 kg/sq.m.
Max power loading 13.6 lb/hp, 6.2 kg/hp.
Load factors +4.5, 2.0 design.

Hornet Microlights Supreme 440 / 440 Dual

The Supreme 440 is identical to the 440 Dual except that the chrome plated joint pieces and electric start are fitted as standard.
While some manufacturers of big engined two seat trikes recommend that ballast should be carried when flying solo, Hornet prefer instead to reduce the throttle opening, saying that, thanks to the lift characteristics of the Cutlass CD wing, the solo pilot can take off quite quickly even on part throttle.

440 Dual
Engine: Robin EC44, 45 hp at 6500 rpm.
Propeller diameter and pitch 54 x 36 inch, 1.37 x 0.91 m.
Toothed belt reduction, ratio 2.5/1.
Max static thrust 270 lb, 122 kg.
Power per unit area 0.23 hp/sq.ft, 2.4hp/sq.m.
Fuel capacity 4.8 US gal, 4.0 Imp gal, 18.2 litre in each tank; two tanks.
Empty weight 293 (313) lb, 133 (142) kg.
Max take off weight 685 lb, 311 kg.
Payload 392 lb, 178 kg.
Max wing loading 3.46 lb/sq.ft, 16.9 kg/sq.m.
Max pow¬er loading 15.2 lb/hp, 6.9 kg/hp.
Load factors; >+3.75 ultimate.
Max level speed 60 mph, 97 kph.
Never exceed speed 68 mph, 109 kph.
Max cruising speed 45 mph, 72 kph.
Economic cruising speed 40 mph, 64 kph.
Stalling speed 26 mph, 42 kph.
Max climb rate at sea level 850 ft/min, 4.3 m/s.
Take off distance 45ft, 14m.
Landing dis¬tance 110ft, 35m (without brakes).
Total range at average cruising speed 190 mile, 306 km.

Supreme 440
Engine: Robin EC44, 45 hp at 6500 rpm.
Propeller diameter and pitch 54 x 36 inch, 1.37 x 0.91 m.
Toothed belt reduction, ratio 2.5/1.
Max static thrust 270 lb, 122 kg.
Power per unit area 0.23 hp/sq.ft, 2.4hp/sq.m.
Fuel capacity 4.8 US gal, 4.0 Imp gal, 18.2 litre in each tank; two tanks.
Empty weight 313 lb, 142 kg.
Max take off weight 705 lb, 320 kg.
Payload 392 lb, 178 kg.
Max wing loading 3.56 lb/sq.ft, 17.4 kg/sq.m.
Max pow¬er loading 15.7 lb/hp, 7.1 kg/hp.
Load factors; >+3.75 ultimate.
Max level speed 60 mph, 97 kph.
Never exceed speed 68 mph, 109 kph.
Max cruising speed 45 mph, 72 kph.
Economic cruising speed 40 mph, 64 kph.
Stalling speed 26 mph, 42 kph.
Max climb rate at sea level 850 ft/min, 4.3 m/s.
Take off distance 45ft, 14m.
Landing dis¬tance 110ft, 35m (without brakes).
Total range at average cruising speed 190 mile, 306 km.

Hornet Microlights Skyhook Sailwings 250/Sabre C

Single seat single engined flex wing aircraft with weight shift control. Rogallo wing with keel pocket. Pilot suspended below wing in trike unit, using bar to control pitch and yaw/roll by altering relative positions of trike unit and wing. Wing braced from above by kingpost and cables, from below by cables; floating cross tube construction with 55% double surface enclosing cross tube; pre-formed ribs. Undercarriage has three wheels in tricycle formation; no suspension on any wheels. Push right go left nosewheel steering independent from yaw control. Optional brake on nosewheel. Aluminium tube trike unit without pod (250), with pod and side fairings (250 Executive). Engine mounted below wing driving pusher propeller. All major components made from aircraft quality materials. Front fork assembly made from aluminium alloy.
The 250 is a basic single seat trike unit generally sold with a Skyhook Sailwings Sabre C wing. Other wings offered are Skyhook Sailwings Cutlass C, Airwave Nimrod, Gold Marque Sports Gyr and Flexiform Skysails Striker.
Instead of the usual bolt and saddle washers method, Hornets use tube joint pieces made from external sleeving, welded together in the appropriate shape (T, L or whatever). The tubes are slid inside the joint pieces and retained by aircraft quality bolts or, for less critical applications, stainless steel rivets. Made from steel, the joint pieces have passivated zinc plating for corrosion protection; chromium plating is an option.
A recognition point is the U shaped nose tube, designed to facilitate the fitting of Hornet’s own glass fibre pod. When fitted with this pod plus glass fibre side fairings, the trike unit is known as the 250 Executive. Other options include a nosewheel brake, alloy skis, alloy wheels, an extra fuel tank holding 3.6 US gal (3.0 Imp Gal).

Horn TH-1

February 1997

Horn TH 1 ZK-TLH was the result of over forty years of experience in aviation by a Levin pilot, being a low wing monoplane similar in microlight configuration to the Bobcat. Powered by a two cylinder Koenig radial, the TH 1 was undergoing ground trials in 1989.

The single-seat aircraft was built by Tom Horn without plans, and features spoilerons rather than ailerons.

It is surprisingly large for a microlight and was re-powered with a 1.8 litre Subaru engine.

ZK-TLH (c/n MAANZ/423) was first registered to Tom Horn of Levin on 17/4/89.

Tom sold it to his cousin Graham Horn of Taupo on 2 September 2002 although Graham may have been operating it for some time before the change of ownership.

Finally, it was sold to Brian Taylor of Whangarei on 2 August 2004. Brian constructed a new cowling and added a turbo charger to the Subaru engine and has flown it quite a bit around the North of the North Island.

Engine: Konig D-1000.
Seats: 1

Horizontec Halcón 1

On 12 March, 2020, it was announced the Halcón 1 MSN 001 aircraft received the Certificate of Airworthiness from the Federal Civil Aviation Agency (AFAC), thus concluding a certification process under the experimental aircraft category.

The two-seater aircraft was built by Horizontec, a Mexican company dedicated to the design and development of aircraft supported by the National Center for Aeronautical Technologies (Centa).
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On September 30th, 2017, the H1 made its first flight at the Queretaro Intercontinental Airport (AIQ), lasting approximately 30 minutes. Subsequently, in February 2018, the aircraft successfully completed 50 flight cycles necessary for Tipo approval, said Giovanni Angelucci, founding partner of Horizontec.

Horgan 1903 Flying Machine

This unusual ornithopter was designed by William C. Horgan together with partners Theophilus Williams and M. Halsinger. It had six wings attached along each side of its five-foot diameter tubular fuselage, intended to make 90 beats per minute driven by a 3.5 hp vapour engine. The framework was made of aluminium and was claimed to weigh only 200 lbs, with the passengers intended to sit in a cage below the fuselage. The machine crashed during a test, putting an end to the Canadian-born Chicago inventor’s dreams of profitable passenger-carrying flights and his plans to participate in the 1904 St Louis Aeronautic Competition.

Hopfner HM-1334 / HM.13/34 / Hirtenberg HM-1334 / HM.13/34

In 1934 Flugzeugbau Hopfner GmbH began building the Hopfner HM.1334 (HM.13/34). This was done on a purely private basis because there was no corresponding request from the Austrian Air Force.

The machine was a two-seat, single-engine biplane in mixed construction with fixed tail wheel gear and normal tail. The fuselage consisted of a tubular steel structure covered with plywood and fabric around the stern. Only in the engine area were light metal sheets used.

The two open pilot seats were arranged one behind the other and had sloped windshields. As engine only a BMW VI with 750 HP was to be used, but there were procurement problems, so that Lampich had to resort to available Fiat A-20 series engines. As armament was a 7.9 mm machine gun Hotchkiss provided, installed in the upper wing and firing over the propeller circle. The biplane wings and the tail were wooden structures covered with plywood and fabric. All control surfaces were cloth-covered. The upper wing had a short wing center piece, which rested on each of two V-struts above the fuselage. The upper and lower wings were each connected by an N-strut and additionally with cables. The tailplane was supported by a strut to the fuselage. The undercarriage was on the engine frame of the fuselage and also backwards to the fuselage and the hull bottom. The wheel arches were aerodynamically shaped.

With the takeover of Hopfner by the Hirtenberger Patronen-, Zündhütchen- and Metallwarenfabrik AG in Hirtenberg, the semi-finished aircraft was brought to Hirtenberg, where it was completed in 1935 and received the designation HM.13/34 or HM.1334.

The first flight took place on June 6, 1935 and during the following flight testing there were no noteworthy incidents. The machine was then presented to the Austrian Air Force, but the interest was low, since several Fw 44J had been procured from Germany for fighter pilot training.

Finally, at the beginning of 1936, three machines were ordered by the Austrian Air Force (for Verwendungsgruppe B, Beanspruchungsgruppe II), which were delivered from the summer of 1936 and received the civil identifiers OE-FAH (factory number 52), OE-FEH (factory number 53) and OE-FIH (factory number 54). After the annexation of Austria to the German Reich in 1938, the three machines, like all Austrian military machines, were taken over by the Luftwaffe and passed on to fighter pilot schools in southern Germany.

The fate of HM.13/34 is unknown.

Hopfner / Hirtenberg HM.13/34
Engine: Fiat A-20, 410 hp (302 kW) max /
Continuous power: 355 hp (282 kW) at 3,000 m
Propeller: adjustable two-bladed wood
Propeller diameter: 2.50 m
Propeller disc: 4.91 m²
Wingspan upper: 10.21 m
Wingspan lower: 9,60 m
Upper wing dihedral: 2.33°
Lower wing dihedral: 2.66°
Wing area: 27.80 m²
Aspect ratio: 6.76
Wing chord: 1.08 m
Length: 8,45 m
Height: 3,03 m
Empty weight: 1,185 kg
Normal weight: 1,585 kg
Maximum TOW: 1,695 kg
Fuel tank capacity: 345 lt
Top speed SL: 258 km / h
Top speed at 3,000 m: 272 km / h
Cruise speed at 3,000 m: 245 km / h
Landing speed: 96 km / h
Ceiling: 6,000 m
Climb rate: 7.3 m / s
Time to 1,000 m: 2,4 min
Time to 3,000 m: 9.5 min
Range normal: 450 km
Maximum range: 600 km
Endurance: 2.5 hr
Wing loading: 60.97 kg / m²
Power load: 4.13 kg / hp (5.61 kg / kW)
Wheel track: 2,54 m
Crew: 1
Armament: 1 x 7.9 mm Hotchkiss machine gun / 500 rounds
Maximum bomb load: 40 kg

Hopfner HS.528

HS.528a

The Hopfner HS-5/28 was a conventional, parasol-wing monoplane utility aircraft built in Austria. It had seating for two occupants in tandem, open cockpits. The landing gear was of fixed, tailskid type with divided main units.

First flying in July 1928, two examples were built with Walter NZ60 engines as HS.528 (HS.5/28) A-50 and A-60 (later received the registration number OE-DLD). The aircraft flew until 1936 in Motorfliegergruppe Wien Nr. 51.

HS.528

Following were two more with the more powerful NZ85, HS.528a (HS.5/28a), one rebuilt HS.528, for the Swiss aeroclub use. The first of the aircraft (the reconstructed A-50, the on-board number CH-231) was delivered to the customer in November 1928, and the second (CH-209) – in March next year. The latter was used until 1934 in the Zurich Aviation Club.

One HS.528a (HS.5/28a) was later 1 rebuilt as an improved version, the HS.829.

HS-5/28a
Engine: 1 × Walter NZ85, 63 kW (85 hp)
Wingspan: 11.26 m (36 ft 11 in)
Wing area: 18.5 m2 (199 ft2)
Length: 7.40 m (24 ft 3 in)
Height: 2.55 m (8 ft 4 in)
Empty weight: 400 kg (880 lb)
Gross weight: 650 kg (1,430 lb)
Maximum speed: 150 km/h (96 mph)
Range: 1,200 km (750 miles)
Crew: One pilot
Capacity: 1 passenger