Engineering:Caspar U.1

From HandWiki
Revision as of 21:07, 4 February 2024 by Corlink (talk | contribs) (change)
(diff) ← Older revision | Latest revision (diff) | Newer revision → (diff)
Short description: Floatplane
Caspar U.1
Caspar U-1.jpg
U.1 under test by the US Navy
Role Submarine-launched patrol seaplane
National origin Germany
Manufacturer Caspar-Werke
Designer Ernst Heinkel
First flight 1922
Primary user Reichsmarine
Number built 3

The Caspar U.1 (sometimes known as the Caspar-Heinkel U.1) was a 1920s Germany patrol seaplane designed by Ernst Heinkel and built by Caspar-Werke.[1] The U.1 was designed to fit into a cylindrical container to allow it to be carried, then launched from a submarine.[1]

Development

The U.1 was designed to meet a requirement to fit inside a cylindrical container 7.40 metres (24.3 ft) long with a diameter of 1.70 m (5 ft 7 in); this allowed the aircraft to be carried by a submarine.[1] To reduce the time to launch the aircraft, it was built as a cantilever biplane to remove the need to rig struts and wires on assembly.[1] The U.1 had two single-step floats and was powered by a front-mounted 55-horsepower (41 kW) Siemens radial piston engine.[1] The pilot had an open cockpit behind the upper wing which gave a clear view forward.[1] It is claimed that during tests, four men could remove the U.1 from the container and erect it in 1 minute 3 seconds.[1] Two aircraft were bought by the United States Navy for evaluation;[1] these were delivered to Naval Air Station Anacostia in late 1922, and were tested during 1923; one of the aircraft was damaged beyond repair whilst mounted on a truck for a parade.[2]

Operators

 Germany
  • Reichsmarine
 United States
  • United States Navy

Specifications

Data from Flight, June 1923[3]

General characteristics

  • Crew: Two
  • Length: 6.20 m (20 ft 4 in)
  • Wingspan: 7.80 m (25 ft 7 in)
  • Height: 2.34 m (7 ft 8 in)
  • Wing area: 14 m2 (150 sq ft)
  • Empty weight: 360 kg (794 lb)
  • Gross weight: 510 kg (1,124 lb)
  • Powerplant: 1 × Siemens 5-cylinder radial engine, 37 kW (50 hp)
  • Propellers: 2-bladed

Performance

  • Maximum speed: 145 km/h (90 mph, 78 kn)
  • Cruise speed: 121 km/h (75 mph, 65 kn)
  • Time to altitude: 7 mins to 1,000 m (3,300 ft)
  • Landing speed: 75 km/h (47 mph; 40 kn)

See also

Aircraft of comparable role, configuration and era

Related lists

References

Notes

  1. 1.0 1.1 1.2 1.3 1.4 1.5 1.6 1.7 Orbis 1985, p. 1060
  2. Treadwell, Terry (February 1983). "Submarine Aviation". Naval Aviation News (Washington, DC: Naval Air Systems Command) 65 (2): 9. ISSN 0028-1417. 
  3. "The Caspar sport seaplane". Flight XV (24): 315–6. 14 June 1923. https://www.flightglobal.com/pdfarchive/view/1923/1923%20-%200315.html. 

Bibliography

  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing. 
  • Herris, Jack (2020). German Aircraft of Minor Manufacturers in WWI: A Centennial Perspective on Great War Airplanes. Gret War Aviation Centennial Series (49). 1: Alter to Korn. n.p.: Aeronaut Books. ISBN 978-1-935881-85-8. 
  • Passingham, Malcolm (February 2000). "Les hydravions embarqués sur sous-marins" (in French). Avions: Toute l'aéronautique et son histoire (83): 7–17. ISSN 1243-8650.