Sputnik 8

''Venera 1'' (russian: Венера-1 meaning ''Venus 1''), also known as Venera-1VA No.2 and occasionally in the West as ''Sputnik 8'' was the first spacecraft to fly past Venus, as part of the Soviet Union's Venera programme. Launched in February 1961, it flew past Venus on 19 May of the same year; however, radio contact with the probe was lost before the flyby, resulting in it returning no data.

Spacecraft

''Venera 1'' was a probe consisting of a cylindrical body in diameter topped by a dome, totalling in height. This was pressurized to with dry nitrogen, with internal fans to maintain even distribution of heat. Two solar panels extended from the cylinder, charging a bank of silver-zinc batteries. A 2-metre parabolic wire-mesh antenna was designed to send data from Venus to Earth on a frequency of 922.8 MHz. A 2.4-metre antenna boom was used to transmit short-wave signals during the near-Earth phase of the mission. Semidirectional quadrupole antennas mounted on the solar panels provided routine telemetry and telecommand contact with Earth during the mission, on a circularly-polarized decimetre radio band.

The probe was equipped with scientific instruments including a flux-gate magnetometer attached to the antenna boom, two ion traps to measure solar wind, micrometeorite detectors, and Geiger counter tubes and a sodium iodide scintillator for measurement of cosmic radiation. An experiment attached to one solar panel measured temperatures of experimental coatings. Infrared and/or ultraviolet radiometers may have been included. The dome contained a KDU-414 engine used for mid-course corrections. Temperature control was achieved by motorized thermal shutters.

During most of its flight, ''Venera 1'' was spin stabilized. It was the first spacecraft designed to perform mid-course corrections, by entering a mode of 3-axis stabilization, fixing on the Sun and the star Canopus. Had it reached Venus, it would have entered another mode of 3-axis stabilization, fixing on the Sun and Earth, and using for the first time a parabolic antenna to relay data.

Launch

''Venera 1'' was the second of two attempts to launch a probe to Venus in February 1961, immediately following the launch of its sister ship ''Venera-1VA No.1'',NSSD
Chronology of Venus Exploration
(NASA Goddard Space Center), accessed August 9, 2010 which failed to leave Earth orbit.NSSD

(NASA Goddard Space Center), accessed August 9, 2010 Soviet experts launched Venera-1 using a Molniya carrier rocket from the Baikonur Cosmodrome. The launch took place at 00:34:36 GMT on 12 February 1961.

The spacecraft, along with the rocket's Blok-L upper stage, was initially placed into a 229 × 282 km low Earth orbit, before the upper stage fired to place "Venera 1" into a heliocentric orbit, directed towards Venus. The 11D33 engine was the world's first staged-combustion-cycle rocket engine, and also the first use of an ullage engine to allow a liquid-fuel rocket engine to start in space.

Failure

Three successful telemetry sessions were conducted, gathering solar-wind and cosmic-ray data near Earth, at the Earth's Magnetopause, and on February 19 at a distance of . After discovering the solar wind with ''Luna 2'', ''Venera 1'' provided the first verification that this plasma was uniformly present in deep space. Seven days later, the next scheduled telemetry session failed to occur. On May 19, 1961, ''Venera 1'' passed within of Venus. With the help of the British radio telescope at Jodrell Bank, some weak signals from ''Venera 1'' may have been detected in June. Soviet engineers believed that ''Venera 1'' failed due to the overheating of a solar-direction sensor.

See also

*List of missions to Venus
*Mariner 2
* Timeline of planetary exploration

References

External links

The Soviet Exploration of VenusNSSDC Master Catalog - ''Venera 1''

{{DEFAULTSORT:Venera 01
Venera program

Spacecraft launched in 1961
Derelict space probes
Derelict satellites in heliocentric orbit
1961 in the Soviet Union
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