Engineering:Akaflieg Karlsruhe AK-5

From HandWiki
Revision as of 18:37, 4 February 2024 by Len Stevenson (talk | contribs) (simplify)
(diff) ← Older revision | Latest revision (diff) | Newer revision → (diff)
Short description: Single-seat German glider, 1990
Akaflieg Karlsruhe AK-5
Akaflieg Karlsruhe AK-5 Neresheim.jpg
AK-5 in Neresheim
Role Club class sailplane
National origin Germany
Manufacturer Akaflieg Karlsruhe
First flight June 1990[1]
Number built 1
Developed into Akaflieg Karlsruhe AK-5b

The AK-5 is a single-seat club class sailplane designed and built in Germany by members of Akaflieg Karlsruhe.

Design and development

AK-5 in the Alps near Timmersdorf

The forward fuselage of the glider was taken from the Glasflügel 604 and the wings were built to the design of the Streifeneder-Hansen Falcon glider, an experimental prototype designed and built by Hansjörg Streifeneder. The cockpit interior was newly designed including a self-designed and built flight director / variometer system and parallelogram control input system similar to Glasflügel practice.[2]

Specifications

Data from [3]

General characteristics

  • Crew: 1
  • Length: 6.8 m (22 ft 4 in)
  • Wingspan: 15 m (49 ft 3 in)
  • Wing area: 10.66 m2 (114.7 sq ft)
  • Aspect ratio: 21.11
  • Airfoil: HQ-21/17.5
  • Empty weight: 278 kg (613 lb)
  • Gross weight: 485 kg (1,069 lb)

Performance

  • Never exceed speed: 270 km/h (170 mph, 150 kn)
  • Maximum glide ratio: 39:1 at 105 km/h (65 mph; 57 kn)
  • Rate of sink: 0.580 m/s (114.2 ft/min) at 85 km/h (53 mph; 46 kn)
  • Wing loading: 45 kg/m2 (9.2 lb/sq ft)

Avionics

  • self-designed flight director / variometer

References

External links