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Pioneer 11

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Template:Short description Template:Use mdy dates Template:Italic title Template:Infobox spaceflight

Pioneer 11 (also known as Pioneer G) is a NASA robotic space probe launched on April 5, 1973, to study the asteroid belt, the environment around Jupiter and Saturn, the solar wind, and cosmic rays.Template:Sfn It was the first probe to encounter Saturn, the second to fly through the asteroid belt, and the second to fly by Jupiter. Later, Pioneer 11 became the second of five artificial objects to achieve an escape velocity allowing it to leave the Solar System. Due to power constraints and the vast distance to the probe, the last routine contact with the spacecraft was on September 30, 1995, and the last good engineering data was received on November 24, 1995.Template:R

Mission background

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History

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Approved in February 1969, Pioneer 11 and its twin probe, Pioneer 10, were the first to be designed for exploring the outer Solar System. Yielding to multiple proposals throughout the 1960s, early mission objectives were defined as:

  • Explore the interplanetary medium beyond the orbit of Mars
  • Investigate the nature of the asteroid belt from the scientific standpoint and assess the belt's possible hazard to missions to the outer planets.
  • Explore the environment of Jupiter.

Subsequent planning for an encounter with Saturn added many more goals:

  • Map the magnetic field of Saturn and determine its intensity, direction, and structure.
  • Determine how many electrons and protons of various energies are distributed along the trajectory of the spacecraft through the Saturn system.
  • Map the interaction of the Saturn system with the solar wind.
  • Measure the temperature of Saturn's atmosphere and that of Titan, the largest satellite of Saturn.
  • Determine the structure of the upper atmosphere of Saturn where molecules are expected to be electrically charged and form an ionosphere.
  • Map the thermal structure of Saturn's atmosphere by infrared observations coupled with radio occultation data.
  • Obtain spin-scan images of the Saturnian system in two colors during the encounter sequence and polarimetry measurements of the planet.
  • Probe the ring system and the atmosphere of Saturn with S-band radio occultation.
  • Determine more precisely the masses of Saturn and its larger satellites by accurate observations of the effects of their gravitational fields on the motion of the spacecraft.
  • As a precursor to the Mariner Jupiter/Saturn mission, verify the environment of the ring plane to find out where it may be safely crossed by the Mariner spacecraft without serious damage.Template:Sfn

Pioneer 11 was built by TRW and managed as part of the Pioneer program by NASA Ames Research Center.Template:R A backup unit, Pioneer H, is currently on display in the "Milestones of Flight" exhibit at the National Air and Space Museum in Washington, D.C.Template:R Many elements of the mission proved to be critical in the planning of the Voyager program.Template:Sfn

Spacecraft design

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The Pioneer 11 bus measures Template:Convert deep and with six Template:Convert panels forming the hexagonal structure. The bus houses propellant to control the orientation of the probe and eight of the twelve scientific instruments. The spacecraft has a mass of 259 kilograms.Template:Sfn

Attitude control and propulsion

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Orientation of the spacecraft was maintained with six 4.5-N,Template:R hydrazine monopropellant thrusters: pair one maintains a constant spin-rate of 4.8 rpm, pair two controls the forward thrust, pair three controls attitude. Information for the orientation is provided by performing conical scanning maneuvers to track Earth in its orbit,Template:R a star sensor able to reference Canopus, and two Sun sensors.Template:Sfn

Communications

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The space probe includes a redundant system transceivers, one attached to the high-gain antenna, the other to an omni-antenna and medium-gain antenna. Each transceiver is 8 watts and transmits data across the S-band using 2110 MHz for the uplink from Earth and 2292 MHz for the downlink to Earth with the Deep Space Network tracking the signal. Prior to transmitting data, the probe uses a convolutional encoder to allow correction of errors in the received data on Earth.Template:Sfn

Power

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File:NASM-NASM2016-00091.jpg
SNAP-19 RTG on a Pioneer 10/11 replica
Pioneer 11 uses four SNAP-19 radioisotope thermoelectric generators (RTGs) (see diagram). They are positioned on two three-rod trusses, each Template:Cvt in length and 120 degrees apart. This was expected to be a safe distance from the sensitive scientific experiments carried on board. Combined, the RTGs provided 155 watts at launch, and decayed to 140 W in transit to Jupiter. The spacecraft requires 100 W to power all systems.Template:Sfn

Computer

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Much of the computation for the mission was performed on Earth and transmitted to the probe, where it is able to retain in memory, up to five commands of the 222 possible entries by ground controllers. The spacecraft includes two command decoders and a command distribution unit, a very limited form of a processor, to direct operations on the spacecraft. This system requires that mission operators prepare commands long in advance of transmitting them to the probe. A data storage unit is included to record up to 6,144 bytes of information gathered by the instruments. The digital telemetry unit is then used to prepare the collected data in one of the thirteen possible formats before transmitting it back to Earth.Template:Sfn

Scientific instruments

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Pioneer 11 has one additional instrument more than Pioneer 10, a flux-gate magnetometer.Template:R

Helium Vector Magnetometer (HVM)
File:Pioneer 10-11 - P50 - fx.jpg Measures the fine structure of the interplanetary magnetic field, mapped the Jovian magnetic field, and provides magnetic field measurements to evaluate solar wind interaction with Jupiter.<ref name=nssdc2/>
Quadrispherical Plasma Analyzer
File:Pioneer 10-11 - P51b - fx.jpg Peer through a hole in the large dish-shaped antenna to detect particles of the solar wind originating from the Sun.<ref name=nssdc3/>
Charged Particle Instrument (CPI)
File:Pioneer 10-11 - P52a - fx.jpg Detects cosmic rays in the Solar System.<ref name=nssdc4/>
Cosmic Ray Telescope (CRT)
File:Pioneer 10-11 - P52b - fx.jpg Collects data on the composition of the cosmic ray particles and their energy ranges.Template:R
Geiger Tube Telescope (GTT)
Template:Center Surveys the intensities, energy spectra, and angular distributions of electrons and protons along the spacecraft's path through the radiation belts of Jupiter and Saturn.Template:R
Trapped Radiation Detector (TRD)
File:Pioneer 10-11 - P54 - fx.jpg

Includes an unfocused Cerenkov counter that detects the light emitted in a particular direction as particles passed through it recording electrons of energy, 0.5 to 12 MeV, an electron scatter detector for electrons of energy, 100 to 400 keV, and a minimum ionizing detector consisting of a solid-state diode that measured minimum ionizing particles (<3 MeV) and protons in the range of 50 to 350 MeV.Template:R

Meteoroid Detectors
File:Pioneer 10-11 - P56 - fx.jpg Twelve panels of pressurized cell detectors mounted on the back of the main dish antenna record penetrating impacts of small meteoroids.Template:R
Asteroid/Meteoroid Detector (AMD)
File:Pioneer 10-11 - P55b - fx.jpg Meteoroid-asteroid detector looks into space with four non-imaging telescopes to track particles ranging from close by bits of dust to distant large asteroids.Template:R
Ultraviolet Photometer
File:Pioneer 10-11 - P57a - fx.jpg Ultraviolet light (200 to 800 Å) is sensed to determine the quantities of hydrogen and helium in space and on Jupiter and Saturn.Template:R
Imaging Photopolarimeter (IPP)
File:Pioneer 10-11 - P60 - fx.jpg The imaging experiment relies upon the spin of the spacecraft to sweep a small telescope across the planet in narrow strips only 0.03 degrees wide, looking at the planet in red (5800 to 7000 Å) and blue (3900 to 4900 Å) light. These strips are then processed to build up a visual image of the planet.Template:R
Infrared Radiometer
File:P58 - fx.jpg Provides information on cloud temperature and the output of heat from Jupiter and Saturn.Template:R
Triaxial Fluxgate Magnetometer
File:Triaxial Fluxgate Mars Global Surveyor Magnetometer.gif Measures the magnetic fields of both Jupiter and Saturn. This instrument is not carried on Pioneer 10.Template:R

Mission profile

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Pioneer 11 launching from Space Launch Complex 36A
Pioneer 11 launching from Launch Complex 36A.

Launch and trajectory

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The Pioneer 11 probe was launched on April 6, 1973, at 02:11:00 UTC, by the National Aeronautics and Space Administration from Space Launch Complex 36A at Cape Canaveral, Florida aboard an Atlas-Centaur launch vehicle, with a Star-37E propulsion module. Its twin probe, Pioneer 10, had been launched on March 3, 1972.

Pioneer 11 was launched on a trajectory directly aimed at Jupiter without any prior gravitational assists.Template:R In May 1974, Pioneer was retargeted to fly past Jupiter on a north–south trajectory, enabling a Saturn flyby in 1979. The maneuver used Template:Cvt of propellant, lasted 42 minutes and 36 seconds, and increased Pioneer 11's speed by 230 km/h.Template:R It also made two mid-course corrections, on April 11, 1973 and November 7, 1974.Template:R Template:-

Encounter with Jupiter

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Template:Main Pioneer 11 flew past Jupiter in November and December 1974. During its closest approach, on December 2, it passed Template:Cvt above the cloud tops. The probe obtained detailed images of the Great Red Spot, transmitted the first images of the immense polar regions, and determined the mass of Jupiter's moon Callisto. Using the gravitational pull of Jupiter, a gravity assist was used to alter the trajectory of the probe towards Saturn and gain velocity. On April 16, 1975, following the Jupiter encounter, the micrometeoroid detector was turned off.Template:R

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Encounter with Saturn

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Template:Main Template:More citations needed section Pioneer 11 passed by Saturn on September 1, 1979, at a distance of Template:Cvt from Saturn's cloud tops.Template:R

By this time, Voyager 1 and Voyager 2 had already passed Jupiter and were en route to Saturn, so it was decided Pioneer 11 would pass through the Saturn ring plane at the same position Voyager 2 would later have to fly through in order to reach Uranus and Neptune. If there were faint ring particles capable of damaging a probe in that area, mission planners felt it was better to learn about it via Pioneer.Template:R Thus, Pioneer 11 was acting as a "pioneer" in a true sense of the word; if danger were detected, then Voyager 2 could be redirected further away from the rings but miss the opportunity to visit the ice giants in the process.

Pioneer 11 imaged—and nearly collided with—one of Saturn's small moons, passing at a distance of no more than Template:Cvt. The object was tentatively identified as Epimetheus, a moon discovered the previous day from PioneerTemplate:'s imaging, and suspected from earlier observations by Earth-based telescopes. After the Voyager flybys, it became known that there are two similarly sized moons (Epimetheus and Janus) in the same orbit, so there is some uncertainty about which one was the object of Pioneer's near-miss. Pioneer 11 encountered Janus on September 1, 1979, at 14:52 UTC, at a distance of Template:Cvt. At 16:20 UTC the same day, Pioneer 11 encountered Mimas at a distance of Template:Cvt.

Besides Epimetheus, instruments located another previously undiscovered small moon and an additional ring, charted Saturn's magnetosphere and magnetic field, and found its planet-sized moon, Titan, to be too cold for life. Hurtling underneath the ring plane, the probe sent back pictures of Saturn's rings. The rings, which normally seem bright when observed from Earth, appeared dark in the Pioneer pictures, and the dark gaps in the rings seen from Earth appeared as bright rings.

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Interstellar mission

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On February 25, 1990, Pioneer 11 became the fourth human-made object to pass beyond the orbit of the planets.Template:R

By 1995, Pioneer 11 could no longer power any of its detectors, so the decision was made to shut it down.Template:R On September 29, 1995, NASA's Ames Research Center, responsible for managing the project, issued a press release that began, "After nearly 22 years of exploration out to the farthest reaches of the Solar System, one of the most durable and productive space missions in history will come to a close." It indicated NASA would use its Deep Space Network antennas to listen "once or twice a month" for the spacecraft's signal, until "some time in late 1996" when "its transmitter will fall silent altogether." NASA Administrator Daniel Goldin characterized Pioneer 11 as "the little spacecraft that could, a venerable explorer that has taught us a great deal about the Solar System and, in the end, about our own innate drive to learn. Pioneer 11 is what NASA is all about – exploration beyond the frontier."Template:R Besides announcing the end of operations, the dispatch provided a historical list of Pioneer 11 mission achievements.

NASA terminated routine contact with the spacecraft on September 30, 1995, but continued to make contact for about two hours every two to four weeks.<ref name=Farewell/> Scientists received a few minutes of good engineering data on November 24, 1995, but then lost final contact once Earth moved out of view of the spacecraft's antenna.Template:R

Timeline

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File:Pioneer speed and distance from Sun.svg
Pioneer 10 and 11 speed and distance from the Sun

Template:Interstellar probes trajectory.svg

Timeline of travel
Date Event
Template:Center Spacecraft launched at 02:11:00.
Template:Center Passage through the asteroid belt.
Template:Center Start Jupiter observation phase.
Time Event
Template:Center Encounter with Jovian system.
Template:Center Callisto flyby at 786,500 km.
Template:Center Ganymede flyby at 692,300 km.
Template:Center
Template:Center Io flyby at 314,000 km.
Template:Center Europa flyby at 586,700 km.
Template:Center Jupiter shadow entry.
Template:Center Jupiter occultation entry.
Template:Center Jupiter closest approach at 42,828 km.
Template:Center Jupiter shadow exit.
Template:Center Jupiter occultation exit.
Template:Center Amalthea flyby at 127,500 km.
Template:Center Phase stop.
Template:Center Start Saturn observation phase.
Time Event
Template:Center Encounter with Saturnian system.
Template:Center Iapetus flyby at 1,032,535 km.
Template:Center Phoebe flyby at 13,713,574 km.
Template:Center
Template:Center Hyperion flyby at 666,153 km.
Template:Center
Template:Center Descending ring plane crossing.
Template:Center Epimetheus flyby at 6,676 km.
Template:Center Atlas flyby at 45,960 km.
Template:Center Dione flyby at 291,556 km.
Template:Center Mimas flyby at 104,263 km.
Template:Center Saturn closest approach at 20,591 km.
Template:Center Saturn occultation entry.
Template:Center Saturn shadow entry.
Template:Center Janus flyby at 228,988 km.
Template:Center Saturn occultation exit.
Template:Center Saturn shadow exit.
Template:Center Ascending ring plane crossing.
Template:Center Tethys flyby at 329,197 km.
Template:Center Enceladus flyby at 222,027 km.
Template:Center Calypso flyby at 109,916 km.
Template:Center Rhea flyby at 345,303 km.
Template:Center
Template:Center Titan flyby at 362,962 km.
Template:Center Phase stop.
Template:Center Begin Pioneer Interstellar Mission.
Template:Center Passed the orbit of Pluto.
Template:Center Routine daily mission operations stopped. Pioneer 11 is 6.5 billion km from Earth.
Template:Center Last signal received.
Template:SfnTemplate:R

Current status

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Due to power constraints and the vast distance to the probe, the last routine contact with the spacecraft was on September 30, 1995, and the last good engineering data was received on November 24, 1995.Template:R

As of June 24, 2024, Pioneer 11 is estimated to be Template:Cvt from the Earth and Template:Convert from the Sun. It was traveling at Template:Cvt relative to the Sun and traveling outward at about 2.35 AU per year.Template:R The spacecraft is heading in the direction of the constellation Scutum near the current position (June 2024) RA 18h 54m dec -8° 46' (J2000.0), close to Messier 26. In 928,000 years, it will pass within Template:Convert of the K dwarf TYC 992-192-1Template:R and will pass near the star Lambda Aquilae in about four million years.Template:R

Pioneer 11 has been overtaken by the two Voyager probes launched in 1977. Voyager 1 has become the most distant object built by humans and will remain so for the foreseeable future, as no probe launched since Voyager has the speed to overtake it.Template:R

Pioneer anomaly

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Template:Main Analysis of the radio tracking data from the Pioneer 10 and 11 spacecraft at distances between 20 and 70 AU from the Sun had consistently indicated the presence of a small but anomalous Doppler frequency drift. The drift can be interpreted as due to a constant acceleration of Template:Nowrap directed towards the Sun. Although it was suspected that there was a systematic origin to the effect, none was found. As a result, there has been sustained interest in the nature of this so-called "Pioneer anomaly".Template:R Extended analysis of mission data by Slava Turyshev and colleagues determined the source of the anomaly to be asymmetric thermal radiation and the resulting thermal recoil force acting on the face of the Pioneers away from the Sun.Template:R

Pioneer plaque

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Template:Main

File:Pioneer10-plaque.jpg
Pioneer plaque

Pioneer 10 and 11 both carry a gold-anodized aluminum plaque in the event that either spacecraft is ever found by intelligent lifeforms from other planetary systems. The plaques feature the nude figures of a human male and female along with several symbols that are designed to provide information about the origin of the spacecraft.Template:R

Commemoration

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In 1991, Pioneer 11 was honored on one of 10 United States Postage Service stamps commemorating uncrewed spacecraft exploring each of the then nine planets and the Moon. Pioneer 11 was the spacecraft featured with Jupiter. Pluto was listed as "Not yet explored".Template:R

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See also

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References

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Bibliography

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