avia.wikisort.org - Aeroplane
The Albatros L102 (company designation) / Albatros Al 102 (RLM designation), was a German trainer aircraft of the 1930s. It was a parasol-wing landplane, seating the student pilot and instructor in separate, open cockpits. A biplane floatplane version was also built as the Al 102W, with strut-braced lower wings.[1]
| L102 | |
|---|---|
 | |
| Role | Trainer |
| Manufacturer | Albatros Flugzeugwerke |
| First flight | September 1932[1] |
| Number built | 10[1] |
Variants
- L102L
- The landplane version with tailwheel undercarriage and parasol monoplane wing. Eight built.[1]
- L102W
- Two examples built as biplane floatplanes, one of which was designated as the Focke-Wulf Fw 55W.[1]
- Al 102L
- RLM designation for the L102L landplane
- Al 102W
- RLM designation for the L102W floatplane
Specifications (L102L)
Data from Die Deutsche Luftrüstung 1933-1945[2] & German Aircraft between 1919 - 1945[1]
General characteristics
- Crew: two
- Length: 8.8 m (28 ft 10 in)
- L102W: 9.4 m (31 ft)
- Wingspan: 13.3 m (43 ft 8 in)
- Height: 3.1 m (10 ft 2 in)
- Wing area: 22.2 m2 (239 sq ft) monoplane
- Al 102W: 31.40 m2 (338 sq ft) (sesquiplane)
- Aspect ratio: 7.97
- Empty weight: 780 kg (1,720 lb)
- L102W: 965 kg (2,127 lb)
- Gross weight: 1,200 kg (2,646 lb)
- L102W: 1,350 kg (2,976 lb)
- Fuel capacity: 160 kg (353 lb) + Oil 20 kg (44 lb)
- L102W: 158 kg (348 lb) + Oil 10 kg (22 lb)
- Powerplant: 1 × Argus As 10C inverted V-8, air-cooled piston engine, 177 kW (237 hp)
Performance
- Maximum speed: 210 km/h (130 mph, 110 kn) at sea level
- L102W: 185 km/h (115 mph; 100 kn) at sea level
- Cruise speed: 195 km/h (121 mph, 105 kn) at sea level
- L102W: 180 km/h (112 mph; 97 kn) at sea level
- Range: 680 km (420 mi, 370 nmi)
- L102W: 585 km (364 mi; 316 nmi)
- Endurance: 3.5 hours
- L102W: 3.25 hours
- Service ceiling: 5,000 m (16,000 ft)
- L102W: 4,500 m (14,764 ft)
- Rate of climb: 4.9 m/s (960 ft/min)
- L102W: 3.1 m/s (610.2 ft/min)
- Wing loading: 54.05 kg/m2 (11.07 lb/sq ft)
- L102W: 42.99 kg/m2 (8.8 lb/ft2)
Notes
- "Albatros Al 102". Germany. Archived from the original on 14 June 2011. Retrieved 9 March 2012.
- Nowarra, Heinz J. (1993). Die Deutsche Luftrüstung 1933-1945 : Band 1 Flugzeugtypen AEG - Dornier (in German). Vol. 1 (1st ed.). Germany: Bernard & Graefe Verlag. pp. 36–37 & 236–237. ISBN 3-7637-5465-2.
References
- Nowarra, Heinz J. (1993). Die Deutsche Luftrüstung 1933-1945 : Band 1 Flugzeugtypen AEG - Dornier (in German). Vol. 1 (1st ed.). Germany: Bernard & Graefe Verlag. pp. 36–37 & 236–237. ISBN 3-7637-5465-2.
External links
Wikimedia Commons has media related to Albatros L 102.
На других языках
[de] Albatros Al 102
Die Albatros Al 102 (Werksbezeichnung L 102) war ein zweisitziges Schulflugzeug der Albatros Flugzeugwerke.[1][2]- [en] Albatros L102
[it] Albatros Al 102
L'Albatros Al 102, o L 102 con la denominazione aziendale pre-RLM, era un monomotore monoplano da addestramento ad ala alta sviluppato dall'azienda aeronautica tedesca Albatros Flugzeugwerke GmbH nei primi anni trenta e prodotto, oltre che dalla stessa, anche dalla Focke-Wulf Flugzeugbau AG.Текст в блоке "Читать" взят с сайта "Википедия" и доступен по лицензии Creative Commons Attribution-ShareAlike; в отдельных случаях могут действовать дополнительные условия.
Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
2019-2025
WikiSort.org - проект по пересортировке и дополнению контента Википедии
WikiSort.org - проект по пересортировке и дополнению контента Википедии