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HPH 304S

HPH 304S

A new glider, a new face!

The new HPH 304S is a single seated, flapped, racing class sailplane. It is offered in a convertible wing configuration with long and short wingtip extensions allowing both 15- and 18-meter wingspans. The glider construction allows assembly of various engine types.

Not simply a face lift of an existing technology, but the very latest in a long study of what was, until now, the “State-of-the-Art”.

The wing

The wing was optimized, calculated from ground up with the help of a research institute and two universities. It incorporates a new thin 13.2% airfoil that is modified in order to reduce the influence of insect contamination. At the root section the wing goes up to 16.4% thickness and meets the fuselage with a refined transition shape. The wing has a special planform with elliptical swept leading edge and special 3D shaped state-of-the-art wingtips, which were optimized to lower the induced drag of the whole wing. The trailing edge incorporates a three section flaperon along its whole length. This configuration brings the pilot friendly behavior and improved flight characteristics.

The tail

The T-shaped tail combines well-proven design with the best possible technology. Elevator and rudder are made with high precision carbon fiber prepreg technology to achieve low weight while keeping high stiffness. Ending tips of the stabilizer have a state-of-the-art shape to raise its efficiency while cutting down the induced drag. Elliptical planform of the stabilizer is a matter of course. Assemblage of the horizontal surface with the vertical is a question of seconds, elevator connects automatically and securing is done by a single pull pin.

The fuselage

Numerous FEM calculations, break tests and simulations of impact behavior resulted in a design that can save life to its pilot. “Roger hook” as a standard feature for safe jettisoning of the canopy is integrated in the massive frame. The middle part of the fuselage is primarily adapted for housing an engine. The motorization program counts with three different engine systems: self launcher, “turbo” sustainer and JET engine. The engine bay and place for fuel tanks are universal for all three systems and are part of the primary structure. Installation of engine can be easily done according to customers demand and can also be done additionally.

Fuselage structure is prepared for engine installation

The cockpit

Comfort in the cockpit has always been one of the main trademarks of Glasflügel sailplanes. The safety cockpit of the 304S has been completely redesigned. Serious design and ergonomic studies have been done to assure perfect seating and view from the cockpit. Every pilot knows how important a feeling of comfort and safety is during the flight. These features were stressed by using materials of the highest quality. Enjoy the massive carbon-aramid frame, prestigious and durable leather interior, well-arranged instrument panel and friendly controls! Every detail has been designed with a special care, check the control-stick handle, canopy lock mechanism or the ventilation outlet! Enough space for elbows and shoulders makes a perfect seating even for taller and heavier pilots. Custom rearrangements are possible of course.

The undercarriage

The 304S is equipped with a spring-loaded and damped landing gear. Double action telescopic frame with rubber shock absorbers in combination with large 5’’ wheel allows cushion-like landing even on a rough field. A hydraulic brake guarantees rapid brake action.

The HPH 304S prototype

The new HPH 304S prototype has been flown in November 2009. Test pilot Ludek Kluger was surprised with the excellent characteristic of the new glider. He reported excellent flying quality from the first moment. Testing will be continued intensively.

Download brochure

Click here to download the electronic brochure for more information on the HPH 304S (PDF file, 3.2 MB).

Read Review

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Elliptical 3D shaped wing tip.

Elliptical 3D shaped wing tip.

Prepreg Elevator and rudder.

Prepreg Elevator and rudder.

Solo sustainer engine. Highly effective TBS 400N jet engine.

Solo sustainer engine. Highly effective TBS 400N jet engine.

The cockpit

The undercarriage

The long travel of the shock absorbing strut provides comfortable landings.

HPH 304S

HPH 304S 18/15m FAI-CLASS Glider Technical Data Sheet

Geometrie

304S 18m

304S 20m **

304SE 15m **

Wing span

18 m | 59 ft

20 m | 65.6 ft

15 m | 49.2 ft

Wing area

11.8 m2 | 127 ft2

12.6 m2 | 135 ft2

8.7 m2 | 94 ft2

Aspect ratio

27.43

31.80

26.37

Fuselage length

6.79 m | 22.28 ft

6.79 m | 22.28 ft

6.79 m | 22.28 ft

Overall height

1.48 m | 4.86 ft

1.48 m | 4.86 ft

1.3 m | 4.3 ft

Fuselage Height

0.83 m | 2.72 ft

0.83 m | 2.72 ft

0.83 m | 2.72 ft

Fuselage Width

0.62 m | 2.03 ft

0.62 m | 2.03 ft

0.62 m | 2.03 ft

Wing Airfoil

HPH xn2 *

HPH xn2 *

HPH xn2 *

Weight

 

 

 

Empty Weight

280 kg | 617 lb

300 kg | 660 lb

230 kg | 507 lb

Maximum Weight

600 kg | 1323 lb

600 kg | 1322 lb

480 kg | 1058 lb

Water ballast

240 l | 66 US gal

240 l | 63 US gal

180 l | 47.6 US gal

Min. Wing Loading

29.6 kg/m2 |
6.0 lb/ft2

30 kg/m2 |
6.1 lb/ft2

34 kg/m2 |
7.5 lb/ft2

Min. Wing Loading

50.8 kg/m2 |
10.4 lb/ft2

47.6 kg/m2 |
9.6 lb/ft2

55 kg/m2 |
12.1 lb/ft2

Leistungen (Segelflug )

 

 

 

Best Glide Ratio

at speed

51

125 km/h | 67.5 kt

> 53

124 km/h | 67 kt

48

123 km/h | 66.5 kt

Min. Sink Rate (min. weight)

at speed

0.45 m/s | 83 ft/min

66 km/h | 36 kt

0.43 m/s | 81 ft/min

68 km/h | 37 kt

0.51 m/s | 100 ft/min

72 km/h | 39 kt

Stall Speed at max. weight

88 km/h | 47.5 kt

85 km/h | 46 kt

87 km/h | 47 kt

VNE

280 km/h | 151 kt

280 km/h | 151 kt

280 km/h | 151 kt

* modified HQ10-16-42, thickness reduced to 13.2%, 16.4% at the root

HPH304MS

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