Venera 10
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Venera 10 orbiter
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| Operator | USSR |
|---|---|
| Mission type | Orbiter and Lander |
| Launch date | June 14, 1975 |
| Launch vehicle | Proton Booster Plus Upper Stage and Escape Stages |
| Satellite of | Venus |
| Orbital insertion date | October 23, 1975 |
| COSPAR ID | 1975-054D |
| Mass | 2300 kg |
| Orbital elements | |
| Eccentricity | .8798 |
| Inclination | 29.5° |
| Apoapsis | 19.82 RV |
| Periapsis | 1.27 RV |
| Orbital period | 49.4 h |
Venera 10 (Russian: Венера-10 meaning Venus 10), manufacturer's designation: 4V-1 No. 661,[1] was a USSR 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).[2]
Contents
Orbiter
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:[3]
- 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
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
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.[3]
It landed 2200 km from Venera 9 (within a 150 km radius of Lua error in package.lua at line 80: module 'strict' not found.), three days after its touchdown.[4] 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.
Lander Payload:[3]
- 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
See also
References
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