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Albatros L102

From Wikipedia, the free encyclopedia
German trainer aircraft
L102
General information
TypeTrainer
ManufacturerAlbatros Flugzeugwerke
Number built10[1]
History
First flightSeptember 1932[1]

TheAlbatros L102 (company designation) /Albatros Al 102 (RLM designation), was a Germantrainer aircraft of the 1930s. It was aparasol-wing landplane, seating the studentpilot and instructor in separate, opencockpits. Abiplanefloatplane version was also built as theAl 102W, withstrut-braced lower wings.[1]

Variants

[edit]
Albatros W 102 photo from L'Aerophile November 1932
  • 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 theFocke-Wulf Fw 55W.[1]
Al 102L
RLM designation for the L102L landplane
Al 102W
RLM designation for the L102W floatplane

Specifications (L102L)

[edit]
Albatros L/W 102 3-view drawing from L'Aerophile November 1932

Data fromDie 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)
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

[edit]
  1. ^abcdef"Albatros Al 102". Germany. Archived fromthe original on 14 June 2011. Retrieved9 March 2012.
  2. ^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

[edit]
  • 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

[edit]
Wikimedia Commons has media related toAlbatros L 102.
Early aircraft
MilitaryIdflieg
designations
B type unarmed reconnaissance biplanes
C type armed reconnaissance biplanes
D typeDoppeldecker fighters
Dr typeDreidecker triplane fighters
G typeGrossflugzeug bombers
J type close support
Company
designations
Landflugzeug (Landplanes)
Wasserflugzeug (Seaplanes)
Höhenflugzeug (High Altitude)
Focke-Wulf aircraft
Company designations, pre-1933
Names
RLM designations, 1933–1945
Company designations, post-1945
Projects
1 to 100
101 to 200
201 to 300
301 to 349
Post-349 (non-sequential)
  • 1 Not assigned
  • 2 Unofficial/proposed
  • 3 Assigned, but not used before RLM was dissolved
  • 4 Assigned to captured aircraft
  • 5 Unconfirmed
  • 6 Propaganda/cover designation
  • 7 Assigned to multiple types

Note: Official RLM designations had the prefix "8-", but this was usually dropped and replaced with the manufacturer's prefix.

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