Venera 1

Venera 1

Venera 1 spacecraft
Mission type Venus flyby
Harvard designation 1961 Gamma 1
SATCAT № 80
Spacecraft properties
Spacecraft 1VA No.2
Manufacturer OKB-1
Launch mass 643.5 kilograms (1,419 lb)
Start of mission
Launch date February 12, 1961, 00:34:36 (1961-02-12UTC00:34:36Z) UTC
Rocket Molniya
Launch site Baikonur 1/5
End of mission
Last contact 19 February 1961 (1961-02-20)
Orbital parameters
Reference system Heliocentric
Flyby of Venus
Closest approach 19 May 1961
Distance 100,000 kilometres (62,000 mi)

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.[1] 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 643.5-kilogram (1,419 lb) probe consisting of a cylindrical body 1.05 metres (3 ft 5 in) in diameter topped by a dome, totalling 2.035 metres (6 ft 8.1 in) in height. This was pressurized to 1.2 standard atmospheres (120 kPa) 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,[2] which failed to leave Earth orbit.[3] Soviet experts launched Venera-1 using a Molniya carrier rocket from the Baikonur Cosmodrome. The launch took place at On 00:34:36 UTC on 12 February 1961.[4]

The spacecraft, along with the rocket's Blok-L upper stage, were initially placed into a 229 × 282 km low Earth orbit,[1] 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 1,900,000 km. 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 100,000 km 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

References

  1. 1 2 NSSDC Spacecraft 1961-003A (NASA Goddard Space Center), accessed August 9, 2010
  2. ↑ NSSDC Chronology of Venus Exploration (NASA Goddard Space Center), accessed August 9, 2010
  3. ↑ NSSDC Tentatively Identified (Soviet) Missions and Launch Failures (NASA Goddard Space Center), accessed August 9, 2010
  4. ↑ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 3 January 2013.

External links

Wikimedia Commons has media related to Venera 1.
This article is issued from Wikipedia - version of the Sunday, November 29, 2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.