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Pioneer Venus Multiprobe

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Pioneer Venus Multiprobe
Artist's impression of the five components of Pioneer 13 approaching Venus
NamesPioneer Venus 2
Pioneer 13
Mission typeVenus atmospheric probes
OperatorNASA / Ames
COSPAR ID1978-078A
SATCAT no.11001
Websitescience.nasa.gov
Mission duration4 months and 1 day
Spacecraft properties
BusHS-507
ManufacturerHughes
Launch mass904 kilograms (1,993 lb)[1]
Dry mass290 kilograms (640 lb) (bus)
315 kilograms (694 lb) (large probe)
3 x 90 kilograms (200 lb) (small probes)
Power241 W
Start of mission
Launch dateAugust 8, 1978, 07:33 (1978-08-08UTC07:33Z) UTC[1]
RocketAtlas SLV-3D Centaur-D1AR (AC-51)
Launch siteCape Canaveral LC-36A
End of mission
Last contactDecember 9, 1978, 20:22:55 UTC
(main bus)
December 9, 1978, 20:55:34 (1978-12-09UTC20:55:35Z) UTC
(Day probe)
Orbital parameters
Reference systemHeliocentric
Semi-major axis0.9 astronomical units (130,000,000 km; 84,000,000 mi)
Eccentricity0.19
Perihelion altitude0.69 astronomical units (103,000,000 km; 64,000,000 mi)
Aphelion altitude1.01 astronomical units (151,000,000 km; 94,000,000 mi)
Inclination2.3 degrees
Period284.0 days
Venus atmospheric probe
Spacecraft componentLarge Probe
Atmospheric entryDecember 9, 1978, 18:45:32 UTC
Impact date19:39:53 UTC
Impact site4°24′N 304°00′E / 4.4°N 304.0°E / 4.4; 304.0
Venus atmospheric probe
Spacecraft componentNorth Probe
Atmospheric entryDecember 9, 1978, 18:49:40 UTC
Impact date19:42:40 UTC
Impact site59°18′N 4°48′E / 59.3°N 4.8°E / 59.3; 4.8
Venus atmospheric probe
Spacecraft componentDay Probe
Atmospheric entryDecember 9, 1978, 18:52:18 UTC
Impact date19:47:59 UTC
Impact site31°18′S 317°00′E / 31.3°S 317.0°E / -31.3; 317.0
Venus atmospheric probe
Spacecraft componentNight Probe
Atmospheric entryDecember 9, 1978, 18:56:13 UTC
Impact date19:52:05 UTC
Impact site28°42′S 56°42′E / 28.7°S 56.7°E / -28.7; 56.7
Venus atmospheric probe
Spacecraft componentMain bus
Atmospheric entryDecember 9, 1978, 20:21:52 UTC

The Pioneer Venus Multiprobe, also known as Pioneer Venus 2 or Pioneer 13, was a spacecraft launched in 1978 to explore Venus as part of NASA's Pioneer program. This part of the mission included a spacecraft bus which was launched from Earth carrying one large and three smaller probes, which after separating penetrated the Venusian atmosphere at a different location, returning data as they descended into the planet's thick atmosphere. The entry occurred on December 9, 1978.

In context

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There was also an orbiter launched in 1978, part of the overall Pioneer Venus project along with this entry probe mission. Whereas the probes entered the atmosphere in 1978, the Pioneer Venus Orbiter would stay in orbit throughout the 1980s and the early 1990s. The next major mission was the Magellan spacecraft, which was an orbiter capable of mapping Venus by seeing through its opaque clouds with radar.

Spacecraft

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Pioneer Venus Bus with probes attached

The Pioneer Venus Multiprobe bus was constructed by the Hughes Aircraft Company, built around the HS-507 bus. It was cylindrical in shape, with a diameter of 2.5 meters (8 ft 2 in) and a mass of 290 kilograms (640 lb). Unlike the probes, which did not begin making direct measurements until they had decelerated lower in the atmosphere, the bus returned data on Venus' upper atmosphere.

The bus was targeted to enter the Venusian atmosphere at a shallow entry angle and transmit data until destruction by the heat of atmospheric friction. The objective was to study the structure and composition of the atmosphere down to the surface, the nature and composition of the clouds, the radiation field and energy exchange in the lower atmosphere, and local information on atmospheric circulation patterns. With no heat shield or parachute, the bus made upper atmospheric measurements with two instruments:

  • BIMS – an ion mass spectrometer to determine the origin and long-term development of the Venusian atmosphere, the dynamics of the upper atmosphere layers, its energy balance and the effect of solar radiation and interplanetary space on those layers. This instrument had a range of 1 to 46 u, used 6 W of power and weighed 5 kilograms (11 lb).
  • BNMS – a neutral mass spectrometer. This made measurements of the interaction between the solar wind and Venus, the photochemistry of the upper layers of and heat distribution in the Venusian atmosphere. It had a range of 1 to 60 u, weighed 1 kilogram (2.2 lb), and used ~1 W of power.

The spacecraft operated down to an altitude of about 110 kilometres (68 mi) before disintegrating.

Probes

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The spacecraft carried one large and three small atmospheric probes, designed by Senior Scientist and Program Manager Irwin Baker of Hughes Aircraft Company, to collect data as they descended into the atmosphere of Venus. The probes did not carry photographic instruments, and were not designed to survive landing – the smaller probes were not equipped with parachutes, and the larger probe's parachute was expected to detach as it neared the ground. All four probes continued transmitting data until impact; however, one survived and continued to transmit data from the surface.

Large probe

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Pioneer Venus Large Probe opens its parachute (artist's rendition)

The large probe carried seven experiments, contained within a sealed spherical pressure vessel. The science experiments were:

  • LNMS – neutral mass spectrometer to measure the atmospheric composition
  • LGC – gas chromatograph to measure the atmospheric composition
  • LSFR – solar flux radiometer to measure solar flux penetration in the atmosphere
  • LIR – infrared radiometer to measure distribution of infrared radiation
  • LCPS – cloud particle size spectrometer to measure particle size and shape
  • LN – nephelometer to search for cloud particles
  • temperature, pressure, and acceleration sensors

This pressure vessel was encased in a nose cone and aft protective cover. After deceleration from initial atmospheric entry at about 11.5 kilometers per second (7.1 mi/s) near the equator on the night side of Venus, a parachute was deployed at 67 kilometres (42 mi) altitude. The large probe was about 150 centimeters (59 in) in diameter and the pressure vessel itself was 73.2 centimeters (28.8 in) in diameter.

Small probes

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A small probe (1-antenna, 2-temperature sensor, 3-frontal protection, 4-hermetic container, 5-nephelometer, 6-radiometer)
Entry of Pioneer Venus Multiprobe (comprising 1 large and 3 small probes)
Pioneer Venus Large Probe descent sequence

Three identical small probes, around 0.8 meters (2 ft 7 in) in diameter, were deployed. These probes consisted of spherical pressure vessels surrounded by an aeroshell, but unlike the large probe, they had no parachutes and the aeroshells did not separate from the probes.

The science experiments were:[2]

  • a neutral mass spectrometer to measure the atmospheric composition
  • a gas chromatograph to measure the atmospheric composition
  • SNFR – solar flux radiometer to measure solar flux penetration in the atmosphere
  • an infrared radiometer to measure distribution of infrared radiation
  • MTUR – cloud particle size spectrometer to measure particle size and shape
  • SN – nephelometer to search for cloud particles
  • SAS – temperature, pressure, and acceleration sensors

The radio signals from all four probes were also used to characterize the winds, turbulence, and propagation in the atmosphere. The small probes were each targeted at different parts of the planet and were named accordingly.[3]

  • The North probe entered the atmosphere at about 60 degrees north latitude on the day side.
  • The Night probe entered on the night side.
  • The Day probe entered well into the day side, and was the only one of the four probes which continued to send radio signals back after impact, for over an hour.

Launch

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The Pioneer Venus Multiprobe was launched by an Atlas SLV-3D Centaur-D1AR rocket, which flew from Launch Complex 36A at the Cape Canaveral Air Force Station. The launch occurred at 07:33 on August 8, 1978, and deployed the Multiprobe into heliocentric orbit for its coast to Venus.

Arrival at Venus

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Prior to the Multiprobe reaching Venus, the four probes were deployed from the main bus. The large probe was released on November 16, 1978, and the three small probes on November 20.

All four probes and the bus reached Venus on December 9, 1978. The large probe was the first to enter the atmosphere, at 18:45:32 UTC, followed over the next 11 minutes by the other three probes. The bus entered the atmosphere at 20:21:52 UTC and returned its last signal at 20:22:55 from an altitude of 110 kilometres (68 mi).

The four probes transmitted data until they impacted the surface of Venus. The Day Probe survived the impact, returning data from the surface for 67 minutes and 37 seconds after reaching the surface.[4]

Pioneer Venus probes and bus: atmospheric entry and impacts (all times in UT)[3]
Entry time (200 km) Impact time Loss of signal Impact coordinates Solar Zenith Angle Local Venus time
Large Probe 18:45:32 19:39:53 19:39:53 4°24′N 304°00′E / 4.4°N 304.0°E / 4.4; 304.0 65.7 7:38
North Probe 18:49:40 19:42:40 19:42:40 59°18′N 4°48′E / 59.3°N 4.8°E / 59.3; 4.8
 108.0 3:35
Day Probe 18:52:18 19:47:59 20:55:34 31°18′S 317°00′E / 31.3°S 317.0°E / -31.3; 317.0
 79.9 6:46
Night Probe 18:56:13 19:52:05 19:52:07 28°42′S 56°42′E / 28.7°S 56.7°E / -28.7; 56.7 150.7 0:07
Bus 20:21:52 (signal lost at 110 km altitude) 20:22:55 37°54′S 290°54′E / 37.9°S 290.9°E / -37.9; 290.9 (estimated) 60.7 8:30

Scientific results

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Below the altitude of 50 kilometres (31 mi) the temperatures measured by the four probes are identical to within a few degrees. They are between 448 and 459 °C (838 and 858 °F) on the surface. The ground pressure is between 86.2 and 94.5 bars (8,620 and 9,450 kPa). Nephelometers identified three cloud layers with different characteristics. The most remarkable discovery was that the ratio of 36argon / 40argon isotopes was much higher than in the Earth's atmosphere, which seems to indicate that the genesis of the Venusian atmosphere is very different from that of Earth. The reconstituted trajectory of the atmospheric probes determined that the wind averaged a speed of 200 metres per second (660 ft/s) in the middle cloud layer at 50 metres per second (160 ft/s) at the base of these clouds and just 1 metre per second (3.3 ft/s) at the ground. Overall data from airborne sensors confirmed, while specifying the data obtained by the Soviet space probe Venera program that preceded this mission.[5]

Trajectory

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Diagram of the PVM's path to planet Venus from Earth in 1978, and this also notes the launch of the Pioneer Venus Orbiter which took place that year also.

Trajectory of Pioneer Venus Multiprobe in 1978

Graphic overview

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Pioneer Venus Multiprobe infographic

See also

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References

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  1. ^ a b "Pioneer Venus Multiprobe/Pioneer Venus 2/Pioneer 13". NASA's Solar System Exploration website. Retrieved December 1, 2022.
  2. ^ "Pioneer Venus Project Information". NASA Goddard Space Flight Center. Retrieved 2016-08-17.
  3. ^ a b Pioneer Venus Probes. NASA Goddard Space Flight Center, 2005.
  4. ^ NASA. Pioneer Venus 2, NASA Science: Solar System Exploration, February 3, 2021. Retrieved 24 April 2022.
  5. ^ Paolo Ulivi et David M. Harland, Robotic Exploration of the Solar System Part 1, The Golden Age 1957–1982, Springer Praxis, 2007 (ISBN 978-0-387-49326-8)

Bibliography

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Wikimedia Commons has media related to Pioneer Venus 2.
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