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H-101 Salto
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| Type designation |
H-101 |
| Competition class |
N/A |
| Number built |
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| Crew |
1 |
| Length |
5.95 m |
| Height |
|
| Cockpit width |
|
| Cockpit height |
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| Wingspan |
13.6 m |
| Wing area |
8.58 m² |
| Aspect ratio |
|
| Wing profile |
FX 66-17 AII-182 |
| Empty mass |
|
| Maximum mass |
280 kg |
| Wing loading |
32.6 kg/m² |
| Maximum speed |
280 km/h |
| Speed in turbulence |
|
| Maneuver speed |
160 km/h |
| Minimum sink rate |
ca. 0.7 m/s at 72 km/h |
| Best glide ratio |
ca. 34 at 90 km/h |
| Acceleration limits |
+7 / -5 g |
The Salto is an aerobatic glider of glass composite construction, developed by Ursula Hänle from the Standard Libelle. The first flight of the prototype took place in March 6, 1970.
[edit] Sources
- German Wikipedia
- Martin Simons, Sailplanes, Vol. 3 1965-1985, EQIP
- Peter Mallinson und Mike Woollard, Handbook of Glider Aerobatics
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