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Venera 5

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COSPAR ID
  
1969-001A

Spacecraft
  
2V (V-69) No.330

Mission duration
  
4.3 months

Launch mass
  
1,130 kg

Rocket
  
Molniya-M

Launch site
  
Baikonur Cosmodrome

SATCAT no.
  
3642

Manufacturer
  
Lavochkin

Dry mass
  
410 kg

Start date
  
January 5, 1969

Operator
  
Lavochkin

Venera 5 wwwpracticalspacecomspacecraftimagesvenera4jpg

Mission type
  
Venus atmospheric probe

Launch date
  
January 5, 1969, 06:28:08 (1969-01-05UTC06:28:08Z) UTC

Venera 5 (Russian: Венера-5 meaning Venus 5) (manufacturer's designation: 2V (V-69)) was a space probe in the Soviet space program Venera for the exploration of Venus.

Contents

Venera 5 was launched towards Venus to obtain atmospheric data. The spacecraft was very similar to Venera 4 although it was of a stronger design. The launch was conducted using a Molniya-M rocket, flying from the Baikonur Cosmodrome.

When the atmosphere of Venus was approached, a capsule weighing 405 kg and containing scientific instruments was jettisoned from the main spacecraft. During satellite descent towards the surface of Venus, a parachute opened to slow the rate of descent. For 53 minutes on May 16, 1969, while the capsule was suspended from the parachute, data from the Venusian atmosphere were returned. It landed at 3°S 18°E. The spacecraft also carried a medallion bearing the State Coat of Arms of the USSR and a bas-relief of V. I. Lenin to the night side of Venus.

Given the results from Venera 4, the Venera 5 and Venera 6 landers contained new chemical analysis experiments tuned to provide more precise measurements of the atmosphere's components. Knowing the atmosphere was extremely dense, the parachutes were also made smaller so the capsule would reach its full crush depth before running out of power (as Venera 4 had done).

Spaceship

  • Instrument KS-18-3M to study the flows of cosmic particles;
  • Instrument LA-2U to determine the distribution of oxygen and hydrogen in the planet's atmosphere.
  • Lander

  • Pressure sensors MDDA A to measure atmospheric pressure in the range of 100 to 30,000 mm Hg. Art. (0.13-40 atm);
  • G-8 gas analyzers to determine the chemical composition of the atmosphere;
  • TTI unit to determine the density of the atmosphere at an altitude;
  • FD-69 for atmospheric lighting measurements;
  • CE-164D to determine the temperature at the height of the atmosphere.
  • References

    Venera 5 Wikipedia