Schleicher ASH 30
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The ASH 30 is a two-seater Open Class glider manufactured by Alexander Schleicher, developed as a replacement for the ASH 25.Script error: No such module "Footnotes".Script error: No such module "Check for unknown parameters". The Mi version is powered by a Script error: No such module "convert". Wankel engine.Script error: No such module "Footnotes".Script error: No such module "Check for unknown parameters". The prototype made its maiden flight on 7 April 2011 from Wasserkuppe.Script error: No such module "Footnotes".Script error: No such module "Check for unknown parameters".
Design and development
The improvements over the ASH 25 are given as:
- a larger span
- new wing sections with a coefficient of lift that is about 0.2 higherScript error: No such module "Footnotes".Script error: No such module "Check for unknown parameters".
- a maximum take-off weight of 850 kg for the Mi version
- automatic control surface connections for the entire aircraft
- enlarged cockpits
- larger canopies to improve visibility and to allow easier entry and exit for the rear pilot
Variants
- ASH 30
- The un-powered prototype glider.
- ASH 30 Mi
- The motor-glider production aircraft, capable of self launching with a retractable engine and propeller.
Specifications (ASH 30 Mi)
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General characteristics
- Crew: Two
- Capacity:
- 50 L (110 lb) max. water ballast in wingTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convert
- Aspect ratio: 40.9Template:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convert
- Fuel capacity:
- 14 L in fuselage fuel tank
- 44 L with 2 wing fuel tanksTemplate:Aircraft specs/convertTemplate:Aircraft specs/engTemplate:Aircraft specs/engTemplate:Aircraft specs/engTemplate:Aircraft specs/lengthTemplate:Aircraft specs/convert
- Propellers: 2-bladedTemplate:Aircraft specs/length
PerformanceTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/rangeTemplate:Aircraft specs/rangeTemplate:Aircraft specs/rangeTemplate:Aircraft specs/convert
- Maximum glide ratio: >60Template:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertScript error: No such module "Check for unknown parameters".
See also
Related lists
Notes
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References
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External links
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