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The Giotto mission was designed to study Comet P/Halley. The major objectives of the mission were to: (1) obtain color photographs of the nucleus; (2) determine the elemental and isotopic composition of volatile components in the cometary coma, particularly parent molecules; (3) characterize the physical and chemical processes that occur in the cometary atmosphere and ionosphere; (4) determine the elemental and isotopic composition of dust particles; (5) measure the total gas-production rate and dust flux and size/mass distribution and derive the dust-to-gas ratio; and, (6) investigate the macroscopic systems of plasma flows resulting from the cometary-solar wind interaction. The spacecraft encountered the comet on March 13, 1986, at a distance of 0.89 AU from the sun and 0.98 AU from the Earth and an angle of 107 degrees from the comet-sun line. The spacecraft was based as much as possible on the ESA-GEOS spacecraft and was spin stabilized with a rate of 15 rpm. During the encounter with Halley's comet, the spin axis was aligned with the relative velocity vector. The 1.5 m dish antenna, operating in the X-band, was inclined and despun in order to point at the Earth (44 degrees with respect to the velocity vector). The goal was to come within 500 km of Halley's comet at closest encounter. The actual closest approach was measured at 596 km.

The main body of Giotto was a short cylinder 1.85 m in diameter by about 1.1 m in length, with three interior platforms. The top platform, 30 cm thick, a main platform, 40 cm, and an experiment platform, 30 cm. Each platform consisted of a disc within the cylinder on which was mounted subsystem and science apparatus. The cylinder was topped by a tripod which surrounded a high gain dish antenna and gave the spacecraft a total height of 2.85 m. The main rocket was positioned in the center of the cylinder with the nozzle protruding out the bottom. The spacecraft had a dust shield consisting of a front sheet of aluminum (1 mm thick) and a 12 mm Kevlar near sheet separated by 25 cm, which could withstand impacts of particles up to 1 gram. The scientific payload was comprised of ten hardware experiments: a narrow-angle camera, three mass spectrometers for neutrals, ions and dust, various dust detectors, a photopolarimeter and a set of plasma experiments. All experiments performed well and returned a wealth of new scientific results, of which perhaps the most important was the clear identification of the cometary nucleus. Fourteen seconds before closest approach, Giotto was hit by a `large' dust particle. The impact caused the spacecraft angular momentum vector to shift by 0.9 degrees, and the spacecraft performed a nutation around the new axis with a period of 16 s and an amplitude of 0.9 degrees; thus, the maximum deviation from the desired attitude was 1.8 degrees. Scientific data were received intermittently for the next 32 minutes. Some experiment sensors suffered damage during this 32-minute interval. Other experiments (the camera baffle and deflecting mirror, the dust detector sensors on the front sheet of the bumper shield, and most experiment apertures) were exposed to dust particles regardless of the accident and also suffered damage. Many of the sensors survived the encounter with little or no damage. Questionable or partially damaged sensors included the camera (later proved to not be functional) and one of the plasma analyzers (RPA). Inoperable experiments included the neutral and ion mass spectrometers and one sensor each on the dust detector and the other plasma analyzer (JPA).

During the Giotto extended mission, the spacecraft flew by the Earth on 2 July 1990 at a distance of 16,300 km at 10:01:18 UTC. This was the first encounter of Earth by a spacecraft coming from deep space. During the encounter, observations were made of the Earth's magnetic field and energetic particles. Giotto obtained a gravitational assist from this flyby and successfully encountered Comet P/Grigg-Skjellerup on July 10, 1992. The closest approach was 200 km at a relative velocity of 13.99 km/s. The heliocentric distance of the spacecraft was 1.01 AU, and the geocentric distance, 1.43 AU at the time of the encounter. The payload was switched on in the evening of July 9. Eight experiments were operated and provided a surprising wealth of exciting data. The Johnstone Plasma Analyser detected the first presence of cometary ions 600,000 km from the nucleus at 12 hours before the closest approach. The Dust Impact Detectors reported the first impact of a fairly large particle at 15:30:56. Bow shocks/waves and acceleration regions were also detected.

On 23 July 1992 Giotto operations were officially terminated after completion of final orbit adjustments and configuration of the spacecraft for its third hibernation. Only 1 to 7 kg of fuel is left on board, insufficient for any extensive future maneuvers. Giotto flew by the Earth on 1 July 1999 at a closest approach of about 219,000 km at approximately 02:40 UT (10:40 p.m. EDT, 30 June). The spacecraft was moving at about 3.5 km/sec relative to Earth.

Spacecraft image for illustrative purposes - not necessarily in the public domain.

Alternate Names

  • 15875
  • urn:esa:psa:context:instrument_host:spacecraft.gio

Facts in Brief

Launch Date: 1985-07-02
Launch Vehicle: Ariane
Launch Site: Kourou, French Guiana
Mass: 582.7 kg
Nominal Power: 196 W

Funding Agency

  • European Space Agency (International)


  • Planetary Science
  • Space Physics

Additional Information

Questions and comments about this spacecraft can be directed to: Dr. David R. Williams



NameRoleOriginal AffiliationE-mail
Dr. Ruedeger ReinhardProject ScientistESA-European Space Research and Technology
Mr. David DaleProject ManagerESA-European Space Research and Technology Centre

Selected References

  • Reinhard, R., The Giotto project, in The Giotto Mission--Its Scientific Investigations, ESA SP-1077, edited by R. Reinhard and B. Battrick, pp. xi-xxv, Mar. 1986.
  • Reinhard, R., The Giotto encounter with comet Halley, Nature, 321, No. 6067, 313-318, doi:10.1038/321313a0, May 1986.
  • Nye, H. R., Giotto: Post-encounter status assessment, ESA J., 12, No. 2, 209-228, 1988.

Halley Information/Data at NSSDCA

Giotto Halley data on CD-ROM
More on the International Halley Watch CD-ROMs

Other International Halley Watch Missions

Vega 1
Vega 2

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