| Pioneer Venus Multiprobe | |||||||||||||||||||||||||||||||||||||||
| Names List: | Pioneer Venus 2 Pioneer 13 | ||||||||||||||||||||||||||||||||||||||
| Mission Type: | Venus atmospheric probes | ||||||||||||||||||||||||||||||||||||||
| Operator: | NASAAmes | ||||||||||||||||||||||||||||||||||||||
| Website: | science.nasa.gov | ||||||||||||||||||||||||||||||||||||||
| Cospar Id: | 1978-078A | ||||||||||||||||||||||||||||||||||||||
| Satcat: | 11001 | ||||||||||||||||||||||||||||||||||||||
| Spacecraft Bus: | HS-507 | ||||||||||||||||||||||||||||||||||||||
| Manufacturer: | Hughes | ||||||||||||||||||||||||||||||||||||||
| Dry Mass: | 290kg (640lb) (bus) 315kg (694lb) (large probe) | ||||||||||||||||||||||||||||||||||||||
| Launch Mass: | 904kg (1,993lb)[1] | ||||||||||||||||||||||||||||||||||||||
| Power: | 241 W | ||||||||||||||||||||||||||||||||||||||
| Launch Date: | UTC | ||||||||||||||||||||||||||||||||||||||
| Launch Rocket: | Atlas SLV-3D Centaur-D1AR | ||||||||||||||||||||||||||||||||||||||
| Launch Site: | Cape Canaveral LC-36A | ||||||||||||||||||||||||||||||||||||||
| Last Contact: | December 9, 1978, 20:22:55 UTC (main bus) UTC (Day probe) | ||||||||||||||||||||||||||||||||||||||
| Orbit Reference: | Heliocentric | ||||||||||||||||||||||||||||||||||||||
| Orbit Semimajor: | 0.9AU | ||||||||||||||||||||||||||||||||||||||
| Orbit Eccentricity: | 0.19 | ||||||||||||||||||||||||||||||||||||||
| Orbit Periapsis: | 0.69AU | ||||||||||||||||||||||||||||||||||||||
| Orbit Apoapsis: | 1.01AU | ||||||||||||||||||||||||||||||||||||||
| Orbit Inclination: | 2.3 degrees | ||||||||||||||||||||||||||||||||||||||
| Orbit Period: | 284.0 days | ||||||||||||||||||||||||||||||||||||||
| Apsis: | helion | ||||||||||||||||||||||||||||||||||||||
| Interplanetary: |
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| Programme: | Pioneer program | ||||||||||||||||||||||||||||||||||||||
| Previous Mission: | Pioneer 12 | ||||||||||||||||||||||||||||||||||||||
| Programme2: | Pioneer Venus | ||||||||||||||||||||||||||||||||||||||
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.
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.
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 2.5m (08.2feet) and a mass of . 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:
The spacecraft operated down to an altitude of about before disintegrating.
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.
The large probe carried seven experiments, contained within a sealed spherical pressure vessel. The science experiments were:
This pressure vessel was encased in a nose cone and aft protective cover. After deceleration from initial atmospheric entry at about 11.5km/s near the equator on the night side of Venus, a parachute was deployed at altitude. The large probe was about 150cm (60inches) in diameter and the pressure vessel itself was 73.2cm (28.8inches) in diameter.
Three identical small probes, around 0.8m (02.6feet) 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]
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 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.
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 110km (70miles).
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]
| 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 | 65.7 | 7:38 | ||
| North Probe | 18:49:40 | 19:42:40 | 19:42:40 | 108.0 | 3:35 | ||
| Day Probe | 18:52:18 | 19:47:59 | 20:55:34 | 79.9 | 6:46 | ||
| Night Probe | 18:56:13 | 19:52:05 | 19:52:07 | 150.7 | 0:07 | ||
| Bus | 20:21:52 | (signal lost at 110 km altitude) | 20:22:55 | (estimated) | 60.7 | 8:30 |
Below the altitude of the temperatures measured by the four probes are identical to within a few degrees. They are between 448and on the surface. The ground pressure is between 86.2and. 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 in the middle cloud layer at at the base of these clouds and just 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]
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.