Hirtenberger HS-9 / Hopfner HS-9 / HS.9/32 / Hirtenburg HS-16

Hirtenberg HS.9A D-EDJH – 12 August 1939

A derivative of the Hopfner HS-5/28 via the Hopfner HS-8/29, the Hirtenberg HS.9 two-seat touring or training aircraft of the late 1920s and early 1930s was an Austrian parasol wing monoplane with a fixed tailskid landing gear and room for two occupants in tandem open cockpits.

Designed by Theodor Hopfner, it had a metal fuselage (front covered with duralumin sheets, the rest – with a cloth) and a wooden wing lined with linen. In the center section there was a fuel tank for 132 liters. The wing consoles, for more convenient storage in the hangar, could be folded along the fuselage.

HS.932

It first flew as the Hopfner HS-9/32 in 1932, powered by a 120 hp de Havilland Gipsy Major I engine. Prototypes HS-9 had civil registration codes A-124 (then changed to OE-ANA) and A-144 (OE-DJH). Later the second prototype was sent to the UK and received the G-AGAK registration there.

Production versions were produced under the designation HS-9/32 (sometimes called the HS-932) and had 150 hp Siemens Sh 14 engines with NACA cowlings and two-bladed screws. As Hopfner’s production facilities were insufficient, HS-9/32 was produced by Hirtenberg Patronen (Hirtenberg), where 9 aircraft were built.

In 1935, four were transferred to the Austrian Air Force for use as training. They were given military registration codes OE-TOH, OE-TUH, OE-TAO and OE-TEO and numbers (Dienst Nummer, DNr.) 426 – 429.

After the annexation of Austria in 1938, several aircraft were still in service. The Germans included captured aircraft in their own air force and left them on Austrian territory, where they were handed over to Nationalsozialistisches Fliegerkorps (NSFK). As of 1939, Gruppe 17 still had five machines of two types: four HS-9/35 with numbers 425-428 and one HS-9 with number 434. As for HS 8/29 (number 412), this aircraft was destroyed in Zeugamt Erding.

A single example of a refined version with an uncowled 125 hp Siemens engine was flown in 1935 as the Hopfner HS-9/35, shortly before the Hopfner company went bankrupt.

HS.9

When Hopfner’s assets were purchased by Otto Eberhardt Patronenfabrik, production continued of both de Havilland- and Siemens-powered (designated HS-9A) aircraft under the Hirtenberg brand.

Hirtenburg HS.9A

Twelve Hopfner HS.932 (HS.9/32) were built from 1932 (2 prototypes + 10 series), including one aircraft with modified ailerons and undercarriage designated as HS.935 / HS.9/35.

In 1935, a significantly modified version of HS-9 \ 35 then in the Fliegertruppen des Osterreichischen Bundesheeres received the code OE-TAR (DNr. 434). With an uncooled Siemens engine it was flown shortly before the Hopfner company went bankrupt.

About 40 were built in total. They were operated by the Austrian Air Force during 1927-1938.

Gallery

Variants
HS-9/32 – Original version by Hopfner
HS-9/35 – developed version of HS-9/32
HS.9 – Production aircraft with a Siemens Sh 14a piston engine.
HS.9A – Production aircraft with a de Havilland Gipsy Major piston engine.
HS.16 – military trainer version of HS.9

HS.9A
Engine: 1 × de Havilland Gipsy Major, 90 kW (120 hp)
Length: 8.05 m (26 ft 5 in)
Wingspan: 10.972 m (36 ft 0 in)
Empty weight: 568.8 kg (1254 lb)
Gross weight: 948 kg (2090 lb)
Maximum speed: 190 km/h (118 mph)
Crew: 2

HS.932
Engine: Siemens Sh 14A, 150 hp
Wing span: 10.96 m
Length: 8.02 m
Height: 2.39 m
Wing area: 18.00 sq.m
Empty weight: 570 kg
Maximum take-off weight: 860 kg
Maximum speed: 190 km / h
Cruising speed: 170 km / h
Practical range: 400 km
Service ceiling: 4400 m
Crew: 2

Hopfner HS-9\35
Engine: Siemens Sh.9, 150 hp
Prop: two-bladed wooden
Wingspan: 10.96 m
Length: 8,02 m
Wing area: 18,00 sq.m
Height: 2.39 m
Empty weight: 570 kg
Takeoff weight: 860 kg
Maximum speed: 190 km / h
Range: 400 km
Ceiling: 4400 m
Crew: 2

HS.9

Hirt Trio

Speed max: 160 mph.
Cruise: 150 mph.
Range: 800 sm.
Stall: 55 mph.
ROC: 850 fpm.
Take-off dist: 950 ft.
Landing dist: 750 ft.
Service ceiling: 21,000 ft.
Engine: Lycoming O-235, 115 hp.
HP range: 115-160.
Fuel cap: 40 USG.
Weight empty: 1050 lbs.
Gross: 1650 lbs.
Height: 6.75 ft.
Length: 21.5 ft.
Wing span: 30 ft.
Wing area: 104.5 sq.ft.
Seats: 2.
Landing gear: nose wheel.

Hipssich 1910 Flieger / Drachenflieger II

The “rekonstruierte Hipssichflieger” – sometimes identified as the Hipssich Drachenflieger II, a development of the I – photographed at the flying field at Wiener Neustadt around the beginning of October 1910. At right, wearing a bowler, is Karl Hipssich. Hippsich was a German inventor living in Vienna with an interest in aviation who invented and patented an automatically stable Flying machine, or “Drachenflieger” rather.

Construction started at the end of 1908 where the actual building was done by the Viennese firm of Karl Köhler. On the left is the pilot of the machine Erich Köhler who had no pilots’ license at the time. He acquired German No. 347 on January 10, 1913 at Breslau when flying a Rumpler Taube.

Hipp’s Superbirds Super Sportster

First flown in 1986, the Super Sportster features detachable wings. In 1997 the kit, including engine, prop and instruments, sold for US$9587, and plans for US$150.

Speed max: 90 mph.
Cruise: 70 mph.
Range: 120 sm.
Stall: 31 mph.
ROC: 800 fpm.
Take-off dist: 50 ft.
Landing dist: 200 ft.
Service ceiling: 12,000 ft.
Engine: Rotax 447, 40 hp.
HP range: 40-50.
Fuel cap: 5 USG.
Weight empty: 260 lbs.
Gross: 550 lbs.
Height: 5.25 ft.
Length: 16.33 ft.
Wing span: 28 ft.
Wing area: 112 sq.ft.
Seats: 1.
Landing gear: tail wheel.

Hipp’s Superbirds Reliant

The Reliant single-seat high-wing LSA microlight was first flown in 1984 and was available for US$6884 in 1997. In 2007 the kit sold for US$9993.
In 1997 the Reliant SX kit sold for US$9587. The price includes engine, prop. And instruments. First flown in 1987, the wings of the SX were also detachable. The Reliant SX is a more powerful version.

Reliant
Speed max: 63 mph.
Cruise: 60 mph.
Range: 120 sm.
Stall: 24 mph.
ROC: 800 fpm.
Take-off dist: 50 ft.
Landing dist: 200 ft.
Service ceiling: 12,000 ft.
Engine: Rotax 277, 28 hp.
HP range: 28-40.
Fuel cap: 5 USG.
Weight empty: 254 lbs.
Gross: 500 lbs.
Height: 5.25 ft.
Length: 16.33 ft.
Wing span: 30 ft.
Wing area: 120 sq.ft.
Cockpit width: 23.6 in
Seats: 1.
Landing gear: tail wheel.

Reliant SX
Speed max: 100 mph.
Cruise: 75 mph.
Range: 120 sm.
Stall: 31 mph.
ROC: 1100 fpm.
Take-off dist: 50 ft.
Landing dist: 150 ft.
Engine: Rotax 447, 40 hp.
HP range: 40-50.
Fuel cap: 5 USG.
Weight empty: 285 lbs.
Gross: 600 lbs.
Height: 5.25 ft.
Length: 16.33 ft.
Wing span: 30 ft.
Wing area: 120 sq.ft.
Seats: 1.
Cockpit width: 23.6 in
Landing gear: tail wheel.

Hipp’s Superbirds J-5 Super Kitten

An LSA with detachable wings, the kit price was US$9387 and plans US$150 in 1997.

Speed max: 90 mph.
Cruise: 70 mph.
Range: 120 sm.
Stall: 31 mph.
ROC: 800 fpm.
Take-off dist: 50 ft.
Landing dist: 200 ft.
Service ceiling: 12,000 ft.
Engine: Rotax 447, 40 hp.
HP range: 40-50.
Fuel cap: 5 USG.
Weight empty: 280 lbs.
Gross: 550 lbs.
Height: 5.25 ft.
Length: 16.33 ft.
Wing span: 30 ft.
Wing area: 120 sq.ft.
Seats: 1.
Landing gear: tail wheel.

Hipp’s Superbirds J-4 Sportster

A single-seat parasol-wing LSA microlight first flown in 1986. Fitted with detachable wings.
The kit price in 1997 was US$6884 and plans US$150. In 2007 the kit price was US$9993 and plans US$250.

Speed max: 63 mph.
Cruise: 59 mph.
Range: 120 sm.
Stall: 24 mph.
ROC: 800 fpm.
Take-off dist: 50 ft.
Landing dist: 200 ft.
Service ceiling: 12,000 ft.
Engine: Rotax 277, 28 hp.
HP range: 28-40.
Fuel cap: 5 USG.
Weight empty: 240 lbs.
Gross: 500 lbs.
Height: 5.25 ft.
Length: 16.33 ft.
Wing span: 28 ft.
Wing area: 112 sq.ft.
Seats: 1.
Landing gear: tail wheel.
Cockpit width: 23.6 in

Hipp’s Superbirds J-3 Kitten

A single-seat, LSA legal high-wing microlight. With detachable wings, the J-3 Kitten first flew in 1986.
The kit price in 1997 was US$6684 and plans US$100.
By 2007 the kit price was US$10,893.

Speed max: 63 mph.
Cruise: 59 mph.
Range: 120-140 sm.
Stall: 24 mph.
ROC: 800 fpm.
Take-off dist: 50 ft.
Landing dist: 200 ft.
Service ceiling: 12,000 ft.
Engine: Rotax 277, 28 hp.
HP range: 28-40.
Fuel cap: 5 USG.
Weight empty: 254 lbs.
Gross: 500 lbs.
Height: 5.25 ft.
Length: 16.3 ft.
Wing span: 30 ft.
Wing area: 120 sq.ft.
Seats: 1.
Landing gear: tail wheel.
Cockpit width: 23.6 in

Hinz BL1-KEA

Top speed: 168 mph
Cruise: 155 mph
Stall: 53 mph
Range: 900 nm
Rate of climb: 790 fpm
Takeoff dist: 1100 ft
Landing dist: 1700 ft
Service ceiling: 12,000 ft
Engine: Limbach, 90 hp
HP range: 90-110
Fuel capacity: 26.4 USG
Empty weight: 1014 lb
Gross weight: 1590 lb
Height: 4.3 ft
Length: 22 ft
Wing span: 32.8 ft
Wing area: 129 sq.ft
Seats: 2
Landing gear: retractable / tail wheel