Glasflügel 401: Difference between revisions
Appearance
Content deleted Content added
Clean up duplicate template arguments using findargdups |
m Replacing old infobox system with Template:Infobox aircraft (via WP:JWB) |
||
(23 intermediate revisions by 16 users not shown) | |||
Line 1: | Line 1: | ||
{{Short description|German single-seat glider, 1968}} |
|||
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
||
{{Infobox aircraft |
|||
| name=401 Kestrel |
| name=401 Kestrel |
||
| image= |
| image=Glasfluegel-401-kestrel-200508.jpg |
||
| caption= |
| caption=Glasflügel 401 Kestrel |
||
⚫ | |||
| type=[[FAI Glider Classes|Open class]] sailplane |
| type=[[FAI Glider Classes|Open class]] sailplane |
||
| |
| national_origin=Germany |
||
| manufacturer=[[Glasflügel]] |
| manufacturer=[[Glasflügel]] |
||
| designer=[[Eugen Hänle]] |
| designer=[[Eugen Hänle]] |
||
| |
| first_flight=9 August 1968 |
||
| |
| introduction= |
||
| retired= |
| retired= |
||
| status= |
| status= |
||
| |
| primary_user= |
||
| |
| number_built=129 |
||
| |
| developed_from= |
||
| variants |
| variants= |
||
}} |
}} |
||
⚫ | |||
|} |
|||
⚫ | |||
==History== |
==History== |
||
Between 1968 and 1975 Glasflügel built 129 ''Kestrels''. |
|||
The ''Kestrel'' can be seen as the prototype of today's [[FAI Glider Classes|18 meter class]]. |
|||
129 ''Kestrel'' gliders were built by Glasflügel between 1968 and 1975. |
|||
⚫ | The British company [[Slingsby Aviation|Slingsby]] |
||
⚫ | The British company [[Slingsby Aviation|Slingsby]] built the ''Kestrel'' under license as the '''T59''' and '''T59B'''. The T59B has a wingspan of 19 metres and was developed for the 1970 [[World Gliding Championships]].<ref>Ellison, Norman (1971), ''British Gliders and Sailplanes'', p.230. A & C Black, Limited, London. {{ISBN|0-7136-1189-8}}</ref> |
||
⚫ | |||
⚫ | On 18 May 2005, Gordon Boettger flew 2061 km in his ''Kestrel'' in [[lee waves]] along the [[Sierra Nevada (U.S.)|Sierra Nevada]] in the USA.<ref>[https://www.fai.org/page/igc-badges-and-diplomas FAI 2000 km Flight Register] {{webarchive|url=https://web.archive.org/web/20111020124415/http://www.fai.org/igc-our-sport/badges-and-diplomas |date=2011-10-20 }} Retrieved 2012-01-02</ref> |
||
<!-- ==Development== --> |
|||
<!-- ==Operational history== --> |
|||
<!-- ==Variants== --> |
|||
<!-- ==Units using this aircraft/Operators (choose)== --> |
|||
==Specifications== |
==Specifications== |
||
⚫ | |||
{{aerospecs |
|||
|prime units? = met |
|||
|ref= |
|||
|met or eng?=<!-- eng for US/UK aircraft, met for all others. You MUST include one or the other here, or no specifications will show -->met |
|||
|crew=One pilot |
|crew=One pilot |
||
|capacity= |
|||
|length m=6.72 |
|length m=6.72 |
||
|length ft=22 |
|length ft=22 |
||
Line 48: | Line 37: | ||
|span ft=55 |
|span ft=55 |
||
|span in=9 |
|span in=9 |
||
|swept m=<!-- swing-wings --> |
|||
|swept ft=<!-- swing-wings --> |
|||
|swept in=<!-- swing-wings --> |
|||
|rot number=<!-- helicopters --> |
|||
|rot dia m=<!-- helicopters --> |
|||
|rot dia ft=<!-- helicopters --> |
|||
|rot dia in=<!-- helicopters --> |
|||
|dia m=<!-- airships etc --> |
|||
|dia ft=<!-- airships etc --> |
|||
|dia in=<!-- airships etc --> |
|||
|width m=<!-- if applicable --> |
|||
|width ft=<!-- if applicable --> |
|||
|width in=<!-- if applicable --> |
|||
|height m= |
|||
|height ft= |
|||
|height in= |
|||
|wing area sqm=11.6 |
|wing area sqm=11.6 |
||
|wing area sqft=125 |
|wing area sqft=125 |
||
|swept area sqm=<!-- swing-wings --> |
|||
|swept area sqft=<!-- swing-wings --> |
|||
|rot area sqm=<!-- helicopters --> |
|||
|rot area sqft=<!-- helicopters --> |
|||
|volume m3=<!-- lighter-than-air --> |
|||
|volume ft3=<!-- lighter-than-air --> |
|||
|aspect ratio=<!-- sailplanes -->25 |
|aspect ratio=<!-- sailplanes -->25 |
||
|empty weight kg=260 |
|empty weight kg=260 |
||
Line 77: | Line 44: | ||
|gross weight kg=400 |
|gross weight kg=400 |
||
|gross weight lb=880 |
|gross weight lb=880 |
||
|lift kg=<!-- lighter-than-air --> |
|||
|lift lb=<!-- lighter-than-air --> |
|||
|eng1 number= |
|||
|eng1 type= |
|||
|eng1 kw=<!-- prop engines --> |
|||
|eng1 hp=<!-- prop engines --> |
|||
|eng1 kn=<!-- jet/rocket engines --> |
|||
|eng1 lbf=<!-- jet/rocket engines --> |
|||
|eng1 kn-ab=<!-- afterburners --> |
|||
|eng1 lbf-ab=<!-- afterburners --> |
|||
|eng2 number= |
|||
|eng2 type= |
|||
|eng2 kw=<!-- prop engines --> |
|||
|eng2 hp=<!-- prop engines --> |
|||
|eng2 kn=<!-- jet/rocket engines --> |
|||
|eng2 lbf=<!-- jet/rocket engines --> |
|||
|eng2 kn-ab=<!-- afterburners --> |
|||
|eng2 lbf-ab=<!-- afterburners --> |
|||
|max speed kmh=250 |
|max speed kmh=250 |
||
|max speed mph=160 |
|max speed mph=160 |
||
|max speed mach=<!-- supersonic aircraft --> |
|||
|cruise speed kmh=<!-- if max speed unknown --> |
|||
|cruise speed mph=<!-- if max speed unknown --> |
|||
|range km= |
|||
|range miles= |
|||
|endurance h=<!-- if range unknown --> |
|||
|endurance min=<!-- if range unknown --> |
|||
|ceiling m= |
|||
|ceiling ft= |
|||
|glide ratio=<!-- sailplanes -->43:1 |
|glide ratio=<!-- sailplanes -->43:1 |
||
|climb rate ms= |
|||
|climb rate ftmin= |
|||
|sink rate ms=<!-- sailplanes --> |
|||
|sink rate ftmin=<!-- sailplanes --> |
|||
|armament1= |
|||
|armament2= |
|||
|armament3= |
|||
|armament4= |
|||
|armament5= |
|||
|armament6= |
|||
}} |
}} |
||
Line 126: | Line 56: | ||
*[[Slingsby Kestrel]] |
*[[Slingsby Kestrel]] |
||
|similar aircraft=<!-- similar or comparable aircraft --> |
|similar aircraft=<!-- similar or comparable aircraft --> |
||
*[[ |
*[[Schleicher ASW 12]] |
||
*[[Schempp-Hirth Cirrus]] |
|||
*[[SZD-38 Jantar 1]] |
*[[SZD-38 Jantar 1]] |
||
|lists=<!-- related lists --> |
|lists=<!-- related lists --> |
||
Line 136: | Line 67: | ||
==References== |
==References== |
||
{{commons category|Kestrel}} |
{{commons category|Glasflügel 401 Kestrel}} |
||
* Flight Manual |
* Flight Manual |
||
* ''Die Entwicklung der Kunststoffsegelflugzeuge'', Dietmar Geistmann, Motorbuchverlag, ISBN |
* ''Die Entwicklung der Kunststoffsegelflugzeuge'', Dietmar Geistmann, Motorbuchverlag, {{ISBN|3-87943-483-2}} |
||
* [http://www.sailplanedirectory.com/ Sailplane Directory] |
* [http://www.sailplanedirectory.com/ Sailplane Directory] |
||
<!-- ==External links== --> |
<!-- ==External links== --> |
||
Line 145: | Line 76: | ||
{{DEFAULTSORT:Glasflugel 401}} |
{{DEFAULTSORT:Glasflugel 401}} |
||
[[Category: |
[[Category:1960s German sailplanes]] |
||
[[Category:German sailplanes 1960–1969]] |
|||
[[Category:Glasflügel aircraft]] |
[[Category:Glasflügel aircraft]] |
||
[[Category:T-tail aircraft]] |
|||
[[Category:Aircraft first flown in 1968]] |
|||
{{aero-1960s-stub}} |
Latest revision as of 00:09, 10 September 2024
401 Kestrel | |
---|---|
General information | |
Type | Open class sailplane |
National origin | Germany |
Manufacturer | Glasflügel |
Designer | |
Number built | 129 |
History | |
First flight | 9 August 1968 |
The Glasflügel 401 "Kestrel" is a glider that was developed in 1968 for the open class. It has a wingspan of 17 metres. It is named after the kestrel bird.
History
[edit]Between 1968 and 1975 Glasflügel built 129 Kestrels.
The British company Slingsby built the Kestrel under license as the T59 and T59B. The T59B has a wingspan of 19 metres and was developed for the 1970 World Gliding Championships.[1]
On 18 May 2005, Gordon Boettger flew 2061 km in his Kestrel in lee waves along the Sierra Nevada in the USA.[2]
Specifications
[edit]General characteristics
- Crew: One pilot
- Length: 6.72 m (22 ft 1 in)
- Wingspan: 17.00 m (55 ft 9 in)
- Wing area: 11.6 m2 (125 sq ft)
- Aspect ratio: 25
- Empty weight: 260 kg (570 lb)
- Gross weight: 400 kg (880 lb)
Performance
- Maximum speed: 250 km/h (160 mph, 140 kn)
- Maximum glide ratio: 43:1
See also
[edit]Related development
Aircraft of comparable role, configuration, and era
Related lists
Notes
[edit]- ^ Ellison, Norman (1971), British Gliders and Sailplanes, p.230. A & C Black, Limited, London. ISBN 0-7136-1189-8
- ^ FAI 2000 km Flight Register Archived 2011-10-20 at the Wayback Machine Retrieved 2012-01-02
References
[edit]Wikimedia Commons has media related to Glasflügel 401 Kestrel.
- Flight Manual
- Die Entwicklung der Kunststoffsegelflugzeuge, Dietmar Geistmann, Motorbuchverlag, ISBN 3-87943-483-2
- Sailplane Directory