H.M. Balloon Factory Delta

An Advisory Committee for Aeronautics was formed in 1909, and a small dirigible, the Baby, was completed and flown. At the end of the year the Balloon School was made a separate establishment with Capper at its head, and the Factory became a civilian unit, although still under War Office direction.

The airship Baby had been rebuilt and improved into the larger Beta, and followed by the progressively larger Gamma and Delta. The first product of the newly established Royal Aircraft Factory was the airship Delta, Naval Airship No.19, which had originally been designed in 1911 as a semi-rigid but emerged in 1912 rebuilt as a non-rigid of 175,000 cu.ft capacity. Contained in a rubberised fabric envelope and powered by two 105 hp White and Poppe engines, driving swivel propellers, it was the fastest British airship so far with a top speed of 45 mph.

A short, 28 foot long car and its crew of five were suspended 20 feet below the envelope, the suspension wires being attached to horizontal ropes sewn into the lower portion of the envelope fabric, while simple brace horizontal and vertical steering surfaces were attached at the stern.

With her increased capacity and a gross lift of 4.6 tons she was extensively used for training and wireless telegraphy experiments conducted by Captain H.Lefroy RE in 1912, during which transmissions were clearly picked up at a range of 100 miles.

Both Gamma and Delta took part in further army war games during 1912 and 1913, where they were employed both in reconnaissance and the ‘bombing’ of towns in ‘enemy’ territory providing valuable experience in the effectiveness of this new weapon for troops and general staff alike.

Engines: 1 x White & Poppe, 110 hp
Capacity: 173,000 cu.ft
Length: 198 ft
Width: 41 ft
Height: 65 ft
Gross lift: 4.8 ton
Disposable lift: 1.46 ton
Speed: 44 mph
Range: 8 hr at cruise
Crew: 5

H.M. Balloon Factory Gamma

An Advisory Committee for Aeronautics was formed in 1909, and a small dirigible, the Baby, was completed and flown. At the end of the year the Balloon School was made a separate establishment with Capper at its head, and the Factory became a civilian unit, although still under War Office direction.

The airship Baby had been rebuilt and improved into the larger Beta, and followed by the progressively larger Gamma of 1910 and Delta. The airship was a considerable advance on Beta both in size and lift capacity, being 152 feet in length and 30 feet in diameter with an initial capacity of 75,000 cu.ft giving a gross lift of 2.1 tons.

The airship Gamma, which had been designed by Colonel Capper, successfully made its maiden flight in February 1910 at Farnborough.

During the army manoeuvres of 1910 HMA Beta and recently completed Gamma were employed in evaluating their potential use to the army in warfare: in extended flights over Somerset, Dorset, Hampshire ad Wiltshire flying reconnaissance sorties; scouting for attacking and defending forces for a period of two months; covering, in the case of Beta, in excess of 1000 miles; spending most nights moored out in the open, using the cover afforded by a screen of trees; being maintained and serviced under these basic conditions, and on one occasion having a broken crankshaft replaced within the protection of a quarry.

During 1911 wireless experiments were carried out with Gamma, where messages were received at ranges of up to 30 miles distant.

Later in 1912 Gamma was reconstructed by lengthening the envelope, increasing the capacity to 101,000 cu.ft and lift to 2.9 tons. In her final form a long, metal-framed car was suspended below a bright yellow rubberised cotton fabric envelope made by the Astra-Torres company in Paris, earning her the nickname the Yellow Peril. Power was supplied by a 35 hp four cylinder, water cooled Green engine driving swivelling propellers mounted on out-riggers from the car, giving her a still air speed of 35 mph.

The swivelling propellers were capable of moving through 240 degrees about her longitudinal axis and were most effective in controlling the ship during climbing and landing. They represented a great technical achievement for the small balloon factory staff at the time.

The envelope was sub-divided by internal tranverse partitions to prevent surging of gas, and had multiple ballonets to preserve envelope pressure.

Capacity: 101,000 cu.ft
Length: 152 ft
Width: 30 ft
Height: 52 ft
Gross lift: 2.9 ton
Disposable lift: 0.5 ton
Engines: 2 x Green 80 hp
Speed: 32 mph
Crew: 5

H.M. Balloon Factory Baby / Beta

Beta, Farnborough 1910

An Advisory Committee for Aeronautics was formed in 1909, and a small dirigible, the Baby, was completed and flown. At the end of the year the Balloon School was made a separate establishment with Capper at its head, and the Factory became a civilian unit, although still under War Office direction.

Launched in May 1909 the 22,000 cu.ft Baby was a more carefully conceived design incorporating some of the more advanced features seen in contemporary continental airships. In its original form the craft was 84 ft in length and 24 ft diameter, with bulbous air-filled fins at the stern. Unlike the earlier Gamma airship, Baby was fitted with an internal ballonet. Power initially came from to inadequate 8 hp Buchet petrol engines, these engines having previously been installed in an early version of the Dunne tail-less biplane.

After initial testing the air-filled fins were replaced with more suitable flat section steering planes, while a 25 hp REP engine was installed to provide more power. After this, and following a series of trials that highlighted poor controllability, she was further taken in hand during the winter. Emerging in the spring of 1910 in a reconstructed form and now known as Beta, her length had been increased to 116 ft with a capacity of 35,000 ft, giving her a gross lift of just over 1 ton together with a greatly improved all-round performance.

A further change of engine, a 35 hp four cylinder, water cooled Green engine, completed the conversion, giving an endurance of five hours with a crew of three.

This small craft was considered the first successful British airship, on one occasion staying aloft for eight hours. She made several flights of note, including flying over London at night in early experiments to determine the best means of defence. Beta was also the first airship to be fitted with a wireless apparatus, being used in early 1911 for experiments succeeding in sending and receiving messages at a distance of over 30 miles.

The airship Baby had been rebuilt and improved into the larger Beta, and followed by the progressively larger Gamma and Delta.

Army Airship Baby – Original configuration of 1909
Dashed outline indicates 1910 enlargement to 104 ft and capacity to 35,000 cu.ft

During the army manoeuvres of 1910 HMA Beta and recently completed Gamma were employed in evaluating their potential use to the army in warfare: in extended flights over Somerset, Dorset, Hampshire ad Wiltshire flying reconnaissance sorties; scouting for attacking and defending forces for a period of two months.

The airship was supported in the field by the old existing balloon gas train and workshop, drawn by a steam traction engine to provide a mobile base.

During the period of the manoeuvres Beta had to be deflated on only one occasion.

In 1912 Beta again underwent further modification, with her envelope being split lengthwise to accommodate an additional longitudinal gore. This increased her diameter to 28 ft and lengthened to 135 ft overall. The swivelling propellers were retained whereas the engine was once more changed, this time to a 45 hp Clerget, increasing the top speed to 35 mph.

Beta was also used in early mooring mast trials; using a mast designed by Commander Masterman RN at Farnborough, known as the ‘high mast’ system, whereby the airship floated free of the ground attached to the mast at the nose, using weighted rollers to keep the stern of the ship in trim as it vaned in the wind.

As Beta II she continued to give good service, taking part in the army war games on Salisbury Plain before the war and being involved in the early parachute experiments carried out from her by General E.M.Maitland.
In January 1914 the navy took over the lighter-than-air operations from the army, with Beta II becoming HMA No.17 and initially used to familiarise naval personel with airship handling.

With the outbreak of war HMA No.17 was for a short time sent to France. Based near Dunkirk, she made several night flights during January 1915 over the German lines and was on artillery-spotting duties before such activities were deemed too dangerous.

Subsequently, HMA No.17 was used for training at RNAS Kingsnorth before finally being deleted in mid-1916.

The non-rigid airship “Baby” was built in 1908-1909, and subsequently enlarged and converted first to the British Army Dirigible No. 3 “Beta I” and then to Naval Airship No. 17 “Beta II”. It survived until 1916, thanks to several major rebuilds and modifications, including four different engine installations. Originally it had three inflatable fins on the tail of the envelope, which were found to be too unwieldy for practical work and were replaced by fixed fins.

1909 Baby
Engine: 2 x Buchet, 8 hp
Capacity: 21,000 ft
Length: 84 ft
Diameter: 26 ft
Height: 38 ft
Gross lift: 0.62 ton
Useful lift: 400 lb
Speed: 20 mph
Endurance: 3 hr
Crew: 3

1910 Baby
Engine: REP, 25 hp
Capacity: 35,000 ft
Length: 104 ft

1910 Baby
Engine: Green, 35 hp
Length: 110 ft
Capacity: 35,000 ft
Endurance: 5 hr
Crew: 3

1912 Beta II
Engine: Clerget, 45 hp
Capacity: 50,000 ft
Length: 116 ft
Width: 28 ft
Height: 40 ft
Gross lift: 1.22 ton
Useful lift: 0.40 ton
Speed: 32 mph
Endurance: 8 hr
Crew: 3

H.M. Balloon Factory Nulli Secundus

Nulli Secundus

The first official government interest began in 1907 at Farnborough where, after receiving a small grant from the War Office of £2000, Colonels Capper and S.F.Cody wre able to start work on the first of the army airships, the Nulli Secundus.

The airship was designed as a semi-rigid and was to be built under conditios of the greatest secrecy. A noticeable feature of the completed craft was the long, uncovered square section metal keel suspended 12 feet below a cylindrical goldbeaters’ skin envelope of 56,000 cu.ft capacity. With a length of 120 ft, power was provided by a 50 hp Antoinette petrol motor, which doubled as the power unit for Cody’s Army Aeroplane No.1, and which drove two aluminium paddle propellers on each side of a small car suspended below the keel containing the crew of three.

An advanced feature of the propellers was that they represented the first use of a variable pitch mechanism in any aircraft, so that the blades coulb be set at an optimum angle of attack. The envelope lacked an internal balloonet compensating for the expansion of gas as the airship rose to a moderate altitude. They did include an automatic gas valve and two hand-operated manoeuvring valves.

The envelope was attached to the keel framework by four circumferential cloth bands and covered with cord netting. The netting bands being made necessary despite the extra weight due to the extreme difficulty of attaching suspension wires or other attachments to the goldbeaters’ skin fabric. Twin rudders were fitted aft, while the elevating plane was situated at the bow in the hope of providing vertical control.

On September 10th, 1907, Nulli Secundus made her maiden flight. A series of short, local flights were made at Farnborough where a speed of 16 mph was obtained.

Following these tests Nulli Secundus departed on 5 October to fly to London, landing after a three and a half hour flight at Crystal Palace. Piloted by Capper and Cody, she set up an endurance record for non rigids by staying in the air for 3.5 hours on the journey from Farnborough to London. The achievement was unfortunately crowned by anti-climax, for excessive headwinds forced the airship down at Crystal Palace on the way back. Strengthening winds threatened to damage the moored ship and the sargent in charge instead ordered the ship to be inflated and it was returned to its base by road.

In December 1907, Cody began to build his first biplane at Farnborough, and Nulli Secundus was being rebuilt to emerge as Nulli Secundus II the following summer.

During the winter month the airship was rebuilt, emerging as Nulli Secundus II of a slightly increased capacity with a new, streamlined silk-covered deep keel that was attached directly to, and faired into, the underside of the envelope. Nulli Secundus II had made its first flight on July 24th, 1908. Several local flights were made during July and August, where a speed of 22 mph was recorded however both vertical and horizontal control was deemed to be inadequate and the airship was dismantled at the end of 1908.

In May 1909, after withdrawing its support for aeroplane experiments, the War Office reorganized the Factory for the primary task of producing airships.

Nulli Secundus II 1908
Capacity: 56,000 cu.ft
Length: 120 ft
Diameter: 26 ft
Height: 44 ft
Gross lift: 1.0 ton
Disposable lift: 0.20 ton
Engine: 1 x Antoinette, 50 hp
Speed: 12 mph
Endurance: 4 hr
Crew: 3

HL Albatron SX

Albatron SX

The tube and fabric two seat Albatros SX could be had with Rotax 582, Rotax 912 or Hirth F 30 engines.

Albatron SX
Engine: Rotax 582 , 64 hp
Wing span: 9.20 m
Wing area: 11 sq.m
MAUW: 450 kg
Empty weight: 255 kg
Fuel capacity: 55 lt
Max speed: 145 kph
Cruise speed: 140 kph
Minimum speed: 65 kph
Climb rate: 4 m/s
Fuel consumption: 12 lt/hr
Certification: VZ
Seats: 2
Price (1998): 54 650 DM vati

HKS 700

700T

The HKS 700E is a twin-cylinder, horizontally opposed, four stroke, carburetted aircraft engine, designed for use on ultralight aircraft, powered parachutes and ultralight trikes. The engine is manufactured by HKS, a Japanese company noted for its automotive racing engines.

The HKS 700E has dual capacitor discharge ignition, dual carburetors and electric start. The engine is mainly air-cooled, but with oil-cooled cylinder heads. The OHV pushrod engine has four valves per cylinder, and nickel-ceramic coated cylinder bores. Lubrication is dry sump, with a trochoid pump.

The reduction drive is a choice of two integral gearboxes: the A-type gearbox has a 2.58:1 ratio and can accommodate propellers of up to 4,000 kg/sq.cm inertial load; the B-type gearbox has a 3.47:1 ratio and can accommodate propellers of up to 6,000 kg/sq.cm.

The 700E burns 9 L (2.4 US gal) per hour in cruise flight at 4,750 rpm. The recommended time between overhauls is 800 hours, although this is expected to be increased as experience is gained.
Producing 60 hp (45 kW) at 6,200 rpm for three minutes for take-off and 56 hp (42 kW) at 5,800 rpm continuously, the 700E was designed as a fuel efficient four stroke alternative to the high fuel consumption two stroke engines, such as the Rotax 582.

HKS 700E

The company’s owner’s manual disclaimer states:
WARNING! This is a non-certified aircraft engine, the possibility of engine failure exists at all times. Do not operate this engine over densely populated areas. Do not operate this engine over terrain where a safe, power off landing cannot be performed. The operating and maintenance instructions supplied with this engine must be followed at all times. Flying any aircraft involves the risk of injury or death, building and maintaining your own aircraft requires great personal responsibility.

Variants:

700E
Initial version, normally aspirated and producing 60 hp (45 kW) at 6200 rpm for three minutes for take-off and 56 hp (42 kW) at 5800 rpm continuously.

700T
Turbocharged version with a 62.5 mm (2.5 in) stroke and a compression ratio of 8.8:1, that produces 80 hp (60 kW) at 5300 rpm for three minutes for take-off and 77 hp (57 kW) at 4900 rpm continuously. The engine’s dry weight is 57.5 kg (127 lb) equipped with electrical system, electric starter, fuel injectors, gearbox, exhaust system and turbocharger. The initial time between overhauls is recommended as 500 hours, but this is expected to rise with operational experience.

700E

Applications:
Aeroalcool Quasar
Aeros del Sur Manta
Aéro Services Guépard Guépe
Air Creation Skypper
Air Creation Trek
Airsport Sonet
Antares MA-33
Aviation Products Star Trike
BAaer Guri
BB Microlight BB-two seater
Bede BD-6
Bede BD-17 Nugget
ASAP Chinook Plus 2
Capella T-Raptor
CGS Hawk
Club ULM Rotor Ptenets-2
Cyclone AX2000
DTA Combo
Earthstar Thunder Gull
Excalibur Aircraft Excalibur
Fletcher Hercules
Flightstar II
Flying K Sky Raider
Flying Machines FM301
Harmening High Flyer
Green Sky Adventures Micro Mong
Hy-Tek Hurricane Hauler
Murphy JDM-8
Murphy Maverick
North Wing Sport X2
Phoenix Air Phoenix
Quad City Challenger
RagWing RW22 Tiger Moth
Rainbow Aerotrike
SlipStream Ultra Sport
Solo Wings Aquilla
Sport Flight Talon
Stellar Astra
Summit Steel Breeze
TechProAviation Merlin 100
Titan Tornado

1998

Specifications:

700E
Type: Two cylinder, four-stroke aircraft engine
Bore: 85 mm (3.3 in)
Stroke: 60 mm (2.4 in)
Displacement: 680 cc (41.49 cu in)
Dry weight: 55 kg (121 lb) equipped with electrical system, electric starter, carburetors, gearbox, exhaust system, oil tank and cooler
Valvetrain: two intake and two exhaust valves per cylinder
Fuel type: unleaded auto fuel
Oil system: dry sump with a trochoid pump
Cooling system: free air cylinders, with oil-cooled cylinder heads
Reduction gear: A-type gearbox with 2.58:1 ratio, limit of 4,000kg/sq.cm inertial load. The B-type gearbox with 3.47:1 ratio, limit of 6,000kg/sq.cm inertial load
Power output: 60 hp (45 kW) at 6200 rpm for three minutes for take-off and 56 hp (42 kW) at 5800 rpm continuous
Compression ratio: 11.3:1
Max torque: 7 kgm at 5800 rpm
Price 1998: $6200

700T
80 HP
Turbo Charged
Intercooled
Elec Fuel Injection
Sea Level Performance at 15,000 ft
Turbo Charged, Electronic Fuel Injection
2 Cylinders 4-Stroke Engine With Horizontally Opposed Cylinders 4 Valves per Cylinder Turbocharger with Intercooler
Bore X Stroke: 85mm x 62.5 mm
Compression Ratio: 8.8 : 1
Power Output: 77hp (57.4kw) at 4900rpm (continuous)
80hp (59.7kw) at 5300rpm (3min./Take off)
Maximum Torque: 79.6 ft lb at 4600 – 5200 rpm
Maximum RPM: 5300
TBO: 500 hours
Reduction Gear: Designation C-type 2.62:1
Engine Weight (Dry, with Electric Starter, Fuel line with Injector, Exhaust Manifold, Intake Manifold, turbocharger, and Gearbox): 126.8 lbs 57.5 kg (57.5 kg)

Hirth Eindecker

Hellmuth Hirth worked for a short time as a foreman at aviation pioneer August Euler in Darmstadt. However, since Euler had difficulties with his Voisin-type flying machine, Hirth returned to Stuttgart to build himself a Blériot machine in 1909. Because of the too weak engine, this did not go beyond small aerial jumps, causing Hirth to go to Vienna to fly the Etrich Taube together with Illner.

Hirth 3701

The Hirth 3701 is an in-line three cylinder, two stroke, carburetted aircraft engine, with optional fuel injection, designed for use on ultralight aircraft and small homebuilts. The 3701 was developed as a liquid-cooled and narrower installation alternative to the four cylinder Hirth F-30 air cooled engine of 85 to 110 hp (63 to 82 kW).

The 3701 features triple Bing 34mm slide carburetors or optionally fuel injection. The cylinder walls are electrochemically coated with Nikasil. Standard starting is electric start and recoil start is not available as an option. The reduction drive system available is the G-50 gearbox, with reduction ratios of 2.16:1, 2.29:1, 2.59:1, 3.16:1, or 3.65:1.

The engine runs on a 50:1 pre-mix of unleaded 93 octane auto fuel and oil, or optionally 100:1 oil injection. The base price in 2009 was US$9815.

Variants:

3701 high torque/low rpm engine
Three-cylinder in-line, two stroke, aircraft engine with three Bing 34mm slide carburetors or fuel injection. Low piston port timing produces 84 hp (63 kW) at 4950 rpm with a very flat torque curve.

3701 high performance engine
Three-cylinder in-line, two stroke, aircraft engine with three Bing 34mm slide carburetors or fuel injection. High piston port timing produces 100 hp (75 kW) at 6000 rpm with a steep torque curve.

Applications:
CGS Hawk II Arrow
Eagle Helicycle
Earthstar Thunder Gull II
Quicksilver MX II
Fusion powered parachute
Infinity powered parachute
InterPlane Skyboy
Rans S-9 Chaos
Skymaster powered parachute
Zenair CH 601 Zodiac

Specifications:

3701 high performance
Type: Three cylinder, two-stroke, in-line, aircraft engine
Bore: 76 mm (3.0 in)
Stroke: 69 mm (2.7 in)
Displacement: 939 cc (57.3 cu in)
Length: 490 mm (19.3 in)
Width: 280 mm (11.0 in)
Height: 420 mm (16.5 in)
Dry weight: 108 lb (49.0 kg), including electric starter and exhaust system. With optional gearbox total weight is 127 lb (57.6 kg), plus radiator.
Valvetrain: piston ported
Fuel system: 3 X Bing 34mm slide type carburetors or fuel injection
Fuel type: unleaded 93 octane auto fuel
Oil system: 50:1 fuel/oil premix or oil injection
Cooling system: liquid
Reduction gear: G-50 gearbox with reduction ratios of 2.16:1, 2.29:1, 2.59:1, 3.16:1, or 3.65:1
Power output: 100 hp (75 kW) at 6000 rpm
Compression ratio: 9.5:1