The Caspar U.1 (sometimes known as the Caspar-Heinkel U.1) was a 1920s German patrol seaplane designed by Ernst Heinkel and built by Caspar-Werke. The U.1 was designed to fit into a cylindrical container to allow it to be carried, then launched from a submarine.
|U.1 under test by the US Navy|
|Role||Submarine-launched patrol seaplane|
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. 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. The U.1 had two single-step floats and was powered by a front-mounted 55-horsepower (41 kW) Siemens radial piston engine. The pilot had an open cockpit behind the upper wing which gave a clear view forward. It is claimed that during tests, four men could remove the U.1 from the container and erect it in 1 minute 3 seconds. Two aircraft were bought by the United States Navy for evaluation; 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.
- 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
- 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)
Aircraft of comparable role, configuration and era
|Wikimedia Commons has media related to Caspar U.1.|
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.