It was a 500 kilograms (1,100 lb) spacecraft, which was built by the Yuzhnoye Design Office, and was used by VNIIEM to conduct experiments with the use of gyroscopes to control spacecraft.[3] Kosmos 14 was the first Soviet experimental weather satellite. The satellite was originally considered to have been orbiting for the purpose of conducting various geophysical studies. However, nearly 4.5 years after its launch, it was specifically identified as a test platform for electrotechnical systems later used to ensure the orientation and stabilization of weather satellites. In addition, tests were made of power supplies using solar cell batteries. The satellite was in the form of a cylinder, with two hemispherical ends, and was 1.8 metres (5 ft 11 in) long and 1.2 metres (3 ft 11 in) in diameter. The control stabilisation system consisted of flywheels driven by electric motors. The kinetic energy of the flywheels was dampened by using electromagnets that produced torque by interacting with the Earth's magnetic field. This system provided three-axis stabilisation and oriented the satellite to Earth. Equipment on board monitored the operation of automatic devices that controlled the solar and chemical batteries. The satellite communicated via a "Mayak" radio transmitter operating at a frequency of 20 MHz. The results of these tests were incorporated in the Kosmos 122 and subsequent launches in the Meteor system. A similar test flight will be made nearly 8 months later with Kosmos 23. These two flights comprised the first stage in the development of Soviet weather satellites.[1]
Kosmos 14 was the first of two Omega satellites to be launched,[3] the other being Kosmos 23.[6] It was operated in an orbit with a perigee of 253 kilometres (157 mi), an apogee of 435 kilometres (270 mi), an inclination of 48.88°, and an orbital period of 91.3 minutes.[2] It remained in orbit until it decayed and reentered the atmosphere on 29 August 1963 after 138 days in orbit.[7]
^ abc"Cosmos 14: Display 1963-010A". nssdc.gsfc.nasa.gov. NASA. 27 February 2020. Retrieved 25 April 2020. This article incorporates text from this source, which is in the public domain.
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets).