Akaflieg Darmstadt D-34 Glider

Compare…

All gliders

Manufacturer
Akaflieg Darmstadt
Description
The Akaflieg Darmstadt D-34 sailplanes were a series of experimental single seat sailplanes, designed at the University of Darmstadt in the 1950s and early 1960s to explore the structural and aerodynamic advantages of the then emerging plastics and composite materials.
First Flight
1955-01-01
Designer
D-34a: W. Sarnes
Length (m)
6.4
Cockpit Crew
1
Min Speed (km/h)
65
National Origin
Germany
Number Built
2
Wikipedia Article (URL)
en.wikipedia.org/wiki/Akaflieg_Darmstadt_D-34
Flat Wing Span (m)
12.65
Flat Wing Area (m²)
9.2
Flat Wing Aspect Ratio
17.5

Related

70 empty fields

Family, Model, Variant, Code Name, IATA Code, ICAO Code, EASA TCDSN, Program Launch, Roll Out, Certification, Entry Into service, Launch Customer, Production End, Service End, Type, Category, Width, Height, Line Logo, White Logo, Max Seating, One Class Typical Seating, Two Class Typical Seating, Three Class Typical Seating, Cargo Volume, Unit Load Devices, Max Speed, Cruise Speed, Optimum Ceiling, Max Ceiling, Rate of Climb, List Price, Armament, Capacity Description, Endurance, Max Mach, Powerplant Description, Primary Users, Status, Projected Wing Span, Projected Wing Area, Projected Wing Aspect Ratio, Wing Sweepback, Wing Flattening, Max Chord, Wing boxes, Wing cells, Wing closed cells, Min Wing Load, Max Wing Load, Wing leading edge material, Wing upper surface material, Wing under surface material, Ribs material, Fuselage Diameter, Cabin Surface, Cabin Diameter, APU, Variable Cost Per Hour, Best Sink Rate, Sink Rate At Best Glide Ratio, Horizontal Speed At Best Glide Ratio, Finesse low estimation, Finesse high estimation, Finesse manufacturer value, EASA Noise Chapter, Lateral Noise Level, Flyover Noise Level, Approac hNoise Level, Cumulative Noise Level