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Galileo (spacecraft)

Galileo was an American robotic space probe that studied the planet Jupiter and its moons, as well as the asteroids Gaspra and Ida. Named after the Italian astronomer Galileo Galilei, it consisted of an orbiter and an entry probe. It was delivered into Earth orbit on October 18, 1989, by Space Shuttle Atlantis, during STS-34. Galileo arrived at Jupiter on December 7, 1995, after gravitational assist flybys of Venus and Earth, and became the first spacecraft to orbit an outer planet.[4]

This article is about the Jupiter probe. For the navigation satellite system, see Galileo (satellite navigation). For the Star Trek shuttle, see Galileo (Star Trek).

Names

Jupiter Orbiter Probe

Jupiter orbiter

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  • Planned: 8 years, 1 month, 19 days
  • Jupiter orbit: 7 years, 9 months, 13 days
  • Final: 13 years, 11 months, 3 days

4,631,778,000 km (2.88 billion mi)[1]

  • Total: 2,560 kg (5,640 lb)[2]
  • Orbiter: 2,220 kg (4,890 lb)[2]
  • Probe: 340 kg (750 lb)[2]

  • Orbiter: 1,880 kg (4,140 lb)[2]
  • Probe: 340 kg (750 lb)[2]

  • Orbiter: 118 kg (260 lb)[2]
  • Probe: 30 kg (66 lb)[2]

  • Orbiter: 570 watts at launch,[2] 493 watts on arrival,[3] 410 watts at end-of-life
  • Probe: 730 watt-hours[2]

October 18, 1989, 16:53:40 (1989-10-18UTC16:53:40) UTC

December 8, 1995, 01:16 UTC SCET

Controlled entry into Jupiter

September 21, 2003, 18:57:18 (2003-09-21UTC18:57:19) UTC

Solid-State Imager

Solid-State Imager

Near-Infrared Mapping Spectrometer

Ultraviolet Spectrometer

Photopolarimeter-Radiometer

Dust Detector Subsystem

Energetic Particles Detector

Heavy Ion Counter

Magnetometer

Plasma Subsystem

Plasma Wave Subsystem

The Jet Propulsion Laboratory built the Galileo spacecraft and managed the Galileo program for NASA. West Germany's Messerschmitt-Bölkow-Blohm supplied the propulsion module. NASA's Ames Research Center managed the atmospheric probe, which was built by Hughes Aircraft Company. At launch, the orbiter and probe together had a mass of 2,562 kg (5,648 lb) and stood 6.15 m (20.2 ft) tall.


Spacecraft are normally stabilized either by spinning around a fixed axis or by maintaining a fixed orientation with reference to the Sun and a star. Galileo did both. One section of the spacecraft rotated at 3 revolutions per minute, keeping Galileo stable and holding six instruments that gathered data from many different directions, including the fields and particles instruments.


Galileo was intentionally destroyed in Jupiter's atmosphere on September 21, 2003. The next orbiter to be sent to Jupiter was Juno, which arrived on July 5, 2016.

Electrical power[edit]

At the time, solar panels were not practical at Jupiter's distance from the Sun; the spacecraft would have needed a minimum of 65 square meters (700 sq ft) of panels. Chemical batteries would likewise be prohibitively large due to technological limitations. The solution was two radioisotope thermoelectric generators (RTGs) which powered the spacecraft through the radioactive decay of plutonium-238. The heat emitted by this decay was converted into electricity through the solid-state Seebeck effect. This provided a reliable and long-lasting source of electricity unaffected by the cold environment and high-radiation fields in the Jovian system.[27][32]


Each GPHS-RTG, mounted on a 5-meter long (16 ft) boom, carried 7.8 kilograms (17 lb) of 238Pu. Each RTG contained 18 separate heat source modules, and each module encased four pellets of plutonium(IV) oxide, a ceramic material resistant to fracturing.[32] The plutonium was enriched to about 83.5 percent plutonium-238.[33] The modules were designed to survive a range of potential accidents: launch vehicle explosion or fire, re-entry into the atmosphere followed by land or water impact, and post-impact situations. An outer covering of graphite provided protection against the structural, thermal, and eroding environments of a potential re-entry into Earth's atmosphere. Additional graphite components provided impact protection, while iridium cladding of the RTGs provided post-impact containment.[32] The RTGs produced about 570 watts at launch. The power output initially decreased at the rate of 0.6 watts per month and was 493 watts when Galileo arrived at Jupiter.[3]

Mission type

1989-084E

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61.4 minutes

340 kg (750 lb)

October 18, 1989 (1989-10-18)

STS-34 piggybacking with Galileo orbiter

Kennedy Space Center, Launch Complex 39B

Termination[edit]

Lacking the fuel to escape Jupiter's gravity well, at the end of Galileo's life, the probe was deliberately crashed into Jupiter on September 21, 2003, to prevent forward contamination of possible life of Jupiter's moon Europa.[68]

1989-084A STS 34

1989-084B Galileo

1989-084C (Orbus 21)

IUS

1989-084D IUS (Orbus 6E)

1989-084E Galileo Probe

The Galileo Probe had COSPAR ID 1989-084E while the orbiter had id 1989-084B.[69] Names for the spacecraft include Galileo Probe or Jupiter Entry Probe abbreviated JEP.[70] The related COSPAR IDs of the Galileo mission were:[71]

Exploration of Jupiter

List of missions to the outer planets

Juno (spacecraft)

Atmosphere of Jupiter

List of spacecraft powered by non-rechargeable batteries

by NASA's Solar System Exploration

Galileo mission site

by NASA's Solar System Exploration

Galileo legacy site

by Arizona State University

Galileo Satellite Image Mosaics

by Kevin M. Gill

Galileo image album

Early probe results report

NASA Space Science Data Coordinated Archive

Galileo Probe