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Venera 10

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Mission type
  
Venus orbiter / lander

SATCAT no.
  
79478423

Manufacturer
  
Inclination
  
29.5°

Launch mass
  
5,033 kg

Operator
  
COSPAR ID
  
1975-054A1975-054D

Spacecraft type
  
4V-1 No. 661

Period
  
2.1 days

Landing mass
  
1,560 kg

Start date
  
June 14, 1975

Launch site
  
Baikonur Cosmodrome

Venera 10 Venera 10 Galleries NASA Solar System Exploration

Mission duration
  
Travel: 4 months and 9 daysLander: 65 minutes

Venera 10 (Russian: Венера-10 meaning Venus 10), manufacturer's designation: 4V-1 No. 661, was a Soviet unmanned space mission to Venus. It consisted of an orbiter and a lander. It was launched on June 14, 1975 03:00:31 UTC and had a mass of 5033 kg (11096 lb).

Contents

Venera 10 Venus Venera 10 Lander

Orbiter

Venera 10 Surface Photographs from Venera 9 and 10

The orbiter entered Venus orbit on October 23, 1975. Its mission was to serve as a communications relay for the lander and to explore cloud layers and atmospheric parameters with several instruments and experiments:

Venera 10 Venera 10 Wikipedia

  • 1.6-2.8 μm IR Spectrometer
  • 8-28 μm IR Radiometer
  • 352 nm UV Photometer
  • 2 Photopolarimeters (335-800 nm)
  • 300-800 nm Spectrometer
  • Lyman-α H/D Spectrometer
  • Bistatic Radar Mapping
  • CM, DM Radio Occultations
  • Triaxial Magnetometer
  • 345-380 nm UV Camera
  • 355-445 nm Camera
  • 6 Electrostatic Analyzers
  • 2 Modulation Ion Traps
  • Low-Energy Proton / Alpha detector
  • Low-Energy Electron detector
  • 3 Semiconductor Counters
  • 2 Gas-Discharge Counters
  • Cherenkov Detector

  • Venera 10 Ninfinger Productions Scale Model Photo Gallery

    The orbiter consisted of a cylinder with two solar panel wings and a high gain parabolic antenna attached to the curved surface. A bell-shaped unit holding propulsion systems was attached to the bottom of the cylinder, and mounted on top was a 2.4 meter sphere which held the landers.

    Lander

    Venera 10 httpsiytimgcomviuyEUxJMTcREmaxresdefaultjpg

    On October 23, 1975, this spacecraft was separated from the Orbiter, and landing was made with the sun near zenith, at 0517 UT, on October 25. A system of circulating fluid was used to distribute the heat load. This system, plus precooling prior to entry, permitted operation of the spacecraft for 65 min after landing. During descent, heat dissipation and deceleration were accomplished sequentially by protective hemispheric shells, three parachutes, a disk-shaped drag brake, and a compressible, metal, doughnut-shaped, landing cushion.

    Venera 10 NASA NSSDCA Spacecraft Details

    It landed near the border area between Beta Regio and Hyndla Regio (within a 150 km radius of 15.42°N 291.51°E / 15.42; 291.51), three days after the touchdown of, and 2200 km from Venera 9. Venera 10 measured a surface windspeed of 3.5 m/s. Other measurements included atmospheric pressure at various heights, and temperature, and surface light levels. Venera 10 was the second probe to send back black and white television pictures from the Venusian surface (after Venera 9). Venera 10 photographs showed lava rocks of pancake shape with lava or other weathered rocks in between. Planned 360 degree panoramic pictures could not be taken because, as with Venera 9, one of two camera lens covers failed to come off, limiting pictures to 180 degrees.

    The lander communicated with Earth using the Venera 10 orbiter as a communication relay.

    Lander Payload:

  • Temperature and pressure sensors
  • Accelerometer
  • Visible / IR photometer - IOV-75
  • Backscatter and multi-angle nephelometers - MNV-75
  • P-11 Mass spectrometer - MAV-75
  • Panoramic telephotometers (2, with lamps)
  • Anemometer - ISV-75
  • Gamma ray spectrometer - GS-12V
  • Gamma ray densitometer - RP-75
  • Radio Doppler experiment
  • References

    Venera 10 Wikipedia