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EXOSAT
	EXOSAT
Mission type	Astronomy
Operator	ESA
COSPAR ID	1983-051A
SATCAT no.	14095
Website	www.esa.int/export/esaSC/120394_index_0_m.html
Mission duration	3 years
Spacecraft properties
Manufacturer	MBB
Launch mass	510.0 kg (1,124.4 lb)
Power	165.0 watts
Start of mission
Launch date	26 May 1983, 15:18:00 UTC
Rocket	Delta 3914 D169
Launch site	Vandenberg SLC-2W
End of mission
Decay date	5 May 1986
Orbital parameters
Reference system	Geocentric
Regime	Low Earth
Eccentricity	0.93428
Perigee altitude	347 km (216 mi)
Apogee altitude	191,709 km (119,122 mi)
Inclination	72.5 degrees
Period	5,435.4 minutes
Epoch	26 May 1983, 11:18:00 UTC
	; Legacy ESA insignia for the EXOSAT mission

The European X-ray Observatory Satellite (EXOSAT), originally named HELOS, was an X-ray telescope operational from May 1983 until April 1986 and in that time made 1780 observations in the X-ray band of most classes of astronomical object including active galactic nuclei, stellar coronae, cataclysmic variables, white dwarfs, X-ray binaries, clusters of galaxies, and supernova remnants.

This European Space Agency (ESA) satellite for direct-pointing and lunar-occultation observation of X-ray sources beyond the Solar System was launched into a highly eccentric orbit (apogee 200,000 km, perigee 500 km) almost perpendicular to that of the Moon on 26 May 1983. The instrumentation includes two low-energy imaging telescopes (LEIT) with Wolter I X-ray optics (for the 0.04–2 keV energy range), a medium-energy experiment using Ar/CO₂ and Xe/CO₂ detectors (for 1.5–50 keV), a Xe/He gas scintillation spectrometer (GSPC) (covering 2–80 keV), and a reprogrammable onboard data-processing computer. Exosat was capable of observing an object (in the direct-pointing mode) for up to 80 hours and of locating sources to within at least 10 arcsec with the LEIT and about 2 arcsec with GSPC.^[2]

History of Exosat

During the period from 1967 to 1969, the European Space Research Organisation (ESRO) studied two separate missions: a European X-ray observatory satellite, as a combined X- and gamma-ray observatory (Cos-A), and a gamma-ray observatory (Cos-B). Cos-A was dropped after the initial study, and Cos-B was proceeded with.

Later in 1969 a separate satellite (the Highly Eccentric Lunar Occultation Satellite - Helos) was proposed. The Helos mission was to determine accurately the location of bright X-ray sources using the lunar occultation technique. In 1973 the observatory part of the mission was added, and mission approval from the European Space Agency Council was given^[3] for Helos, now renamed Exosat.

It was decided that the observatory should be made available to a wide community, rather than be restricted to instrument developers, as had been the case for all previous ESA (ESRO) scientific programmes. For the first time in an ESA project, this led to the approach of payload funding and management by the Agency. Instrument design and development became a shared responsibility between ESA and hardware groups.

In July 1981 ESA released the first Announcement of Opportunity (AO) for participation in the Exosat observation programme to the scientific community of its Member States. By 1 November 1981, the closing of the AO window, some 500 observing proposals had been received. Of these, 200 were selected for the first nine months of operation.^[2]

Exosat was the first ESA spacecraft to carry on board a digital computer (OBC), with its main purpose being scientific data processing. Spacecraft monitoring and control were secondary. To provide the data handling subsystem with an exceptional flexibility of operation, the OBC and Central Terminal Unit were in-flight reprogrammable. This flexibility far exceeded any other ESA spacecraft built up to then.

Satellite operations

Each of the three axes were stabilized and the optical axes of the three scientific instruments were coaligned. The entrance apertures of the scientific instruments were all located on one face of the central body. Once in orbit the flaps which cover the entrances to the ME and LEIT were swung open to act as thermal and stray-light shields for the telescopes and star trackers, respectively.^[2]

The orbit of Exosat was different from any previous X-ray astronomy satellite. To maximize the number of sources occulted by the Moon, a highly eccentric orbit (e ~ 0.93) with a 90.6 hr period and an inclination of 73° was chosen.^[4] The initial apogee was 191,000 km and perigee 350 km. To be outside the Earth's radiation belts, the scientific instruments were operated above ~50,000 km, giving up to ~76 hr per 90 hr orbit.^[4] There was no need for any onboard data storage as Exosat was visible from the ground station at Villafranca, Spain for practically the entire time the scientific instruments were operated.

References

^ "EXOSAT". NASA Space Science Data Coordinated Archive. NASA. Retrieved October 23, 2017.
^ ^a ^b ^c Hoff HA (Aug 1983). "EXOSAT - The new extrasolar X-ray observatory". J Brit Interplan Soc. (Space Chronicle). 36 (8): 363–7. Archived from the original on 2012-08-29.
^ Taylor BG, Andresen RD, Peacock A, Zobl R (Mar 1981). "The Exosat mission". Space Sci. Rev. 30 (1–4): 479–94. Bibcode:1981SSRv...30..479T. doi:10.1007/BF01246069. S2CID 120475350.
^ ^a ^b White NE, Peacock A (1988). "The Exosat observatory". Societa Astronomica Italiana, Memorie. 59 (1–2): 7–31. Bibcode:1988MmSAI..59....7W.