Giotto (spacecraft)

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An image of the Giotto spacecraft during construction Giotto Whipple shield ESA239195.jpg
An image of the Giotto spacecraft during construction

The cylindrical spacecraft was 1.85 m in diameter and had three internal platforms. It was derived from the GEOS research satellite built by British Aerospace in Filton, Bristol, and modified with the addition of a dust shield (Whipple shield) as proposed by Fred Whipple. The shield comprised a thin (1 mm) aluminium sheet separated by a space and a thicker (12 mm) Kevlar sheet. [3] The later Stardust spacecraft would use a similar Whipple shield. Giotto also had a 1.51 m diameter antenna that it used to communicate with Earth. [3] A mock-up of the spacecraft resides at the Bristol Aero Collection hangar, at Filton, Bristol, England.[ citation needed ]

Science Instruments

Giotto had 10 science instruments. [4] [5]

  • MAG: a magnetometer
  • HMC (Halley Multicolour Camera): a 16-cm telescope and camera
  • DID (Dust Impactor Detector System): measured the mass of dust particles that hit the instrument
  • RPA (Rème Plasma Analyser): studied solar wind and charged particles
  • JPA (Johnstone Plasma Analyser): also measured solar wind and charged particles
  • PIA (Particulate Impact Analyser): studied the size and chemistry of particles
  • OPE (Optical Probe Experiment): examined the emissivity of gas and dust behind the spacecraft
  • EPA (Energetic Particle Analyser): analyzed alpha-particles, electrons, and neutrons
  • NMS (Neutral Mass Spectrometer): measured the composition of the particles around the comet
  • IMS (Ion Mass Spectrometer): measured the amount of ions from the sun and the comet
  • GRE (Giotto Radio Experiment): used Giotto's radio signals to study Halley's comet

Timeline

Launch

The mission was given the go-ahead by ESA in 1980, and launched on an Ariane 1 rocket (flight V14) on 2 July 1985 from Kourou, French Guiana. The craft was controlled from the European Space Agency ESOC facilities in Darmstadt (then West Germany) initially in Geostationary Transfer Orbit (GTO) then in the Near Earth Phase (NEP) before the longer Cruise Phase through to the encounter. While in GTO a number of slew and spin-up manoeuvres (to 90 RPM) were carried out in preparation for the firing of the Apogee Boost Motor (ABM), although unlike orbit circularisations for geostationary orbit, the ABM for Giotto was fired at perigee. Attitude determination and control used sun pulse and IR Earth sensor data in the telemetry to determine the spacecraft orientation.

Halley encounter

The Soviet Vega 1 started returning images of Halley on 4 March 1986, and the first ever of its nucleus, and made its flyby on 6 March, followed by Vega 2 making its flyby on 9 March. Vega 1's closest approach to Halley was 8889 km.

Giotto passed Halley successfully on 14 March 1986 at 596 km distance, and surprisingly survived despite being hit by some small particles. One impact sent it spinning off its stabilized spin axis so that its antenna no longer always pointed at the Earth, and its dust shield no longer protected its instruments. After 32 minutes Giotto re-stabilized itself and continued gathering science data.

Another impact destroyed the Halley Multicolor Camera, but not before it took photographs of the nucleus at closest approach.

Comet Halley at Giotto spacecraft's closest approach Comet Halley close up.jpg
Comet Halley at Giotto spacecraft's closest approach

First Earth flyby

Giotto's trajectory was adjusted for an Earth flyby and its science instruments were turned off on 15 March 1986 at 02:00 UTC.

Grigg–Skjellerup encounter

Giotto was commanded to wake up on 2 July 1990 when it flew by Earth in order to sling shot to its next cometary encounter.

The probe then flew by the Comet Grigg–Skjellerup on 10 July 1992 which it approached to a distance of about 200 km. Afterwards, Giotto was again switched off on 23 July 1992.

Second Earth flyby

In 1999 Giotto made another Earth flyby but was not reactivated.

Scientific results

Images showed Halley's nucleus to be a dark peanut-shaped body, 15 km long, 7 km to 10 km wide. Only 10% of the surface was active, with at least three outgassing jets seen on the sunlit side. Analysis showed the comet formed 4.5 billion years ago from volatiles (mainly ice) that had condensed onto interstellar dust particles. It had remained practically unaltered since its formation.

Measured volume of material ejected by Halley:

Giotto found Halley's nucleus was dark, which suggested a thick covering of dust. [6]

The nucleus's surface was rough and of a porous quality, with the density of the whole nucleus as low as 0.3 g/cm3. [6] Sagdeev's team estimated a density of 0.6 g/cm3, [7] but S. J. Peale warned that all estimates had error bars too large to be informative. [8]

The quantity of material ejected was found to be three tonnes per second [9] for seven jets, and these caused the comet to wobble over long time periods. [6]

The dust ejected was mostly only the size of cigarette smoke particles, with masses ranging from 10 ag to 0.4 g. (See Orders of magnitude (mass).) The mass of the particle that impacted Giotto and sent it spinning was not measured, but from its effects—it also probably broke off a piece of Giotto [9] —the mass has been estimated to lie between 0.1 g and 1 g. [6]

Two kinds of dust were seen: one with carbon, hydrogen, nitrogen and oxygen; the other with calcium, iron, magnesium, silicon and sodium. [6]

The ratio of abundances of the comet's light elements excluding nitrogen (i.e. hydrogen, carbon, oxygen) were the same as the Sun's. The implication is that the constituents of Halley are among the most primitive in the Solar System.

The plasma and ion mass spectrometer instruments showed Halley has a carbon-rich surface.

Spacecraft achievements

  • Giotto made the closest approach to Halley's Comet and provided the best data for this comet. [10]
  • Giotto was the first spacecraft:
  • to provide detailed pictures of a cometary nucleus. [11]
  • to make a close flyby of two comets. Young and active comet Halley could be compared to old comet 26P/Grigg–Skjellerup.
  • to return from interplanetary space and perform an Earth swing-by.
  • to be re-activated from hibernation mode.
  • to use Earth for a gravity assist. [12]

See also

Notes

  1. "Giotto" (PDF). NASA. Retrieved 30 November 2022.
  2. "NSSDCA Master Catalog – Giotto – Trajectory Details". nssdc.gsfc.nasa.gov. NASA . Retrieved 21 June 2016.
  3. 1 2 "Giotto Whipple shield". www.esa.int. Retrieved 21 January 2022.
  4. "Giotto – PSA – Cosmos". www.cosmos.esa.int. Retrieved 19 January 2022.
  5. "ESA Science & Technology – Instruments". sci.esa.int. Retrieved 19 January 2022.
  6. 1 2 3 4 5 "ESA Science & Technology: Halley". ESA. 10 March 2006. Retrieved 22 February 2009.
  7. RZ Sagdeev; PE Elyasberg; VI Moroz (1988). "Is the nucleus of Comet Halley a low density body?". Nature. 331 (6153): 240. Bibcode:1988Natur.331..240S. doi:10.1038/331240a0. S2CID   4335780.
  8. S. J. Peale (November 1989). "On the density of Halley's comet". Icarus . 82 (1): 36–49. Bibcode:1989Icar...82...36P. doi:10.1016/0019-1035(89)90021-3.
  9. 1 2 J. A. M. McDonnell; et al. (15 May 1986). "Dust density and mass distribution near comet Halley from Giotto observations". Nature. 321 (6067s): 338–341. Bibcode:1986Natur.321..338M. doi:10.1038/321338a0. S2CID   122092751.
  10. Curdt, W.; Wilhelm, K.; Craubner, A.; Krahn, E.; Keller, H. U. (February 1988). "Position of comet P/Halley at the Giotto encounter". Astronomy and Astrophysics. 191 (1): L1–L3. Bibcode:1988A&A...191L...1C. ISSN   0004-6361.
  11. Keller, H. U.; Arpigny, C.; Barbieri, C.; Bonnet, R. M.; Cazes, S.; Coradini, M.; Cosmovici, C. B.; Delamere, W. A.; et al. (15 May 1986). "First Halley Multicolour Camera imaging results from Giotto". Nature. 321 (6067s): 320–326. Bibcode:1986Natur.321..320K. doi:10.1038/321320a0. S2CID   120631677.
  12. Siddiqi, Asif A. (2018). Beyond Earth: A Chronicle of Deep Space Exploration, 1958–2016 (PDF). The NASA history series (second ed.). Washington, DC: NASA History Program Office. p. 2. ISBN   9781626830424. LCCN   2017059404. SP2018-4041.
Giotto
Giotto spacecraft.jpg
Artist's concept of Giotto spacecraft
Operator European Space Agency
COSPAR ID 1985-056A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 15875
Website Official Site at ESA.int
Mission duration7 years and 1 month (launch to deactivation)
Spacecraft properties
Launch mass960 kg [1]
Power196 W
Start of mission
Launch date11:23:00,2 July 1985(UTC) (1985-07-02T11:23:00Z)
Rocket Ariane 1
Launch site Guiana Space Centre
End of mission
Deactivated23 July 1992 (1992-07-23)
Orbital parameters
Reference system Heliocentric [2]
Eccentricity 0.17334
Perihelion altitude 0.73 AU
Aphelion altitude 1.04 AU
Inclination 2.09°
Period 304.6 days
Epoch 10 July 1992, 15:18:43 UTC
Flyby of Comet Halley
Closest approach14 March 1986
Distance596 km (370 mi)

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