Grob G104 Speed Astir: Difference between revisions
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{{Short description|Competition sailplane built by Grob Aircraft, 1978}} |
{{Short description|Competition sailplane built by Grob Aircraft, 1978}} |
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|manufacturer=[[Grob Aircraft]] |
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|designer=[[Burkhart Grob]] |
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|first flight=April 1978 |
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The '''Grob G104 Speed Astir''' was a competition sailplane produced in Germany in the late 1970s as [[Grob Aircraft|Grob]]'s first design in the [[15 metre class]]. Taking the [[Grob G 102 Astir|G102 Astir]] design as a starting point, the Speed Astir featured a new wing of narrower chord and different section, a fin and rudder of reduced height, capacity for 150 kg (330 lb) of water ballast, and "elastic flaps". This latter feature eliminated the drag normally associated with the air gap between the wing and a deployed flap. It did this by extending the wing skin over the entire upper surface so the highly flexible skin served as the flap hinge and there was no air gap between the flap and the remainder of the wing. |
The '''Grob G104 Speed Astir''' was a competition sailplane produced in Germany in the late 1970s as [[Grob Aircraft|Grob]]'s first design in the [[15 metre class]]. Taking the [[Grob G 102 Astir|G102 Astir]] design as a starting point, the Speed Astir featured a new wing of narrower chord and different section, a fin and rudder of reduced height, capacity for 150 kg (330 lb) of water ballast, and "elastic flaps". This latter feature eliminated the drag normally associated with the air gap between the wing and a deployed flap. It did this by extending the wing skin over the entire upper surface so the highly flexible skin served as the flap hinge and there was no air gap between the flap and the remainder of the wing. |
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Revision as of 20:30, 16 April 2021
 | This article includes a list of general references, but it lacks sufficient corresponding inline citations. (December 2012) |
| G104 Speed Astir and Speed Astir II | |
|---|---|
| |
| Speed Astir IIb in flight | |
| Role | 15 metre class sailplane |
| National origin | Germany |
| Manufacturer | Grob Aircraft |
| Designer | Burkhart Grob |
| First flight | April 1978 |
| Number built | 108 |
The Grob G104 Speed Astir was a competition sailplane produced in Germany in the late 1970s as Grob's first design in the 15 metre class. Taking the G102 Astir design as a starting point, the Speed Astir featured a new wing of narrower chord and different section, a fin and rudder of reduced height, capacity for 150 kg (330 lb) of water ballast, and "elastic flaps". This latter feature eliminated the drag normally associated with the air gap between the wing and a deployed flap. It did this by extending the wing skin over the entire upper surface so the highly flexible skin served as the flap hinge and there was no air gap between the flap and the remainder of the wing.
The original Speed Astir flew in early 1978, but was replaced in production by the end of the year by a refined design named the Speed Astir II. This had a slimmer, laminar-flow fuselage and made use of carbon fibre in its construction. A version with a lengthened fuselage for taller pilots and incorporating carbon fibre wing spars was made available in 1979 as the IIB, along with an increased-span version of the IIB as the II 17.5. Production of all variants was discontinued shortly thereafter.
Specifications (Speed Astir II)
General characteristics
- Crew: One pilot
- Length: 6.69 m (21 ft 11 in)
- Wingspan: 15.00 m (49 ft 3 in)
- Height: 1.27 m (4 ft 2 in)
- Wing area: 11.5 m2 (124 sq ft)
- Aspect ratio: 19.6
- Empty weight: 265 kg (584 lb)
- Gross weight: 515 kg (1,135 lb)
Performance
- Maximum speed: 270 km/h (168 mph, 146 kn)
- Maximum glide ratio: 41.5
- Rate of sink: 0.60 m/s (120 ft/min)
See also
Aircraft of comparable role, configuration, and era
References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 441.
- Hardy, Michael (1982). Gliders and Sailplanes of the World. Shepperton: Ian Allan. pp. 49–50.
- Homepage of Grob Aircraft