Date: 2 Jul 1985
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).
Image Credit: NSSDC