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European Retrievable Carrier

From Wikipedia, the free encyclopedia

European Retrievable Carrier
Eureca ESA382424.jpg
EURECA deployment in 1992
Mission typeMaterials science
Astronomy
OperatorESA
COSPAR ID1992-049B
SATCAT no.22065
Mission durationPlanned: 1 year
Elapsed: 334 days
Spacecraft properties
ManufacturerMBB-ENRO
Launch mass4,491 kilograms (9,901 lb)
Power1,000 watts
Start of mission
Launch date31 July 1992, 11:56:48 UTC
RocketSpace Shuttle Atlantis
STS-46
Launch siteKennedy LC-39B
Deployment date2 August 1992 (1992-08-02)
End of mission
DisposalRecovered
Recovered bySpace Shuttle Endeavour
STS-57
Recovery date1 July 1993 (1993-08)
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Eccentricity0.00066
Perigee altitude438 kilometres (272 mi)
Apogee altitude447 kilometres (278 mi)
Inclination28.5 degrees
Period93.4 minutes
Epoch2 August 1992, 20:00:00 UTC[1]
 

The European Retrievable Carrier (EURECA) was an unmanned 4.5-tonne satellite with 15 experiments.[2] It was a European Space Agency (ESA) mission and the acronym was derived from Archimedes' bathtub revelation "Eureka!".

It was built by the German MBB-ERNO and had automatic material science cells as well as small telescopes for solar observation (including x-ray).

It was launched 31 July 1992 by Space Shuttle Atlantis during STS-46, and placed into an orbit at an altitude of 508 km (316 mi). EURECA was retrieved on 1 July 1993 by Space Shuttle Endeavour during STS-57 and returned to Earth. It was designed to fly five times with different experiments but the following flights were cancelled.

EURECA is one of the few unmanned space vehicles that have been returned to the Earth unharmed. It has been on display at the Swiss Museum of Transport in Lucerne since 2000.[3]

Design

EURECA retrieval in 1993
EURECA retrieval in 1993

EURECA was made of high-strength carbon-fiber struts and titanium nodal points joined together to form a framework of cubic elements. Thermal control on EURECA combined both active and passive heat transfer and radiation systems. Active heat transfer was achieved by means of a freon cooling loop which dissipated the thermal load through two radiators into space. The passive system made use of multilayer insulation blankets combined with electrical heaters.

The electrical subsystem was powered by deployable and retractable solar arrays together with four 40 amp-hour nickel-cadmium batteries. When EURECA was in the Shuttle cargo bay, power was supplied by the Shuttle. The modular attitude and orbit control subsystem (AOCS) maintained attitude and spacecraft orientation and stabilization. An orbit transfer assembly, consisting of four thrusters, was used to boost EURECA to its operational attitude of 515 km (320 mi) and return it to a retrievable orbit of about 300 km (190 mi).

EURECA was three-axis stabilized by means of a magnetic torque assembly together with a nitrogen reaction control assembly (RCA). Data handling was carried out by EURECAs data handling subsystem (DHS) supported by telemetry and command subsystems providing the link to the ground station.

Experiments

EURECA consisted of 15 experiments:[4][5]

  • Solution Growth Facility (SGF) (Belgium, Denmark, Norway) BelgiumDenmarkNorway
  • Protein Crystallization Facility (PCF) (Germany) Germany
  • Exobiology Radiation Assembly (ERA) (Germany) Germany
  • Multi-Furnace Assembly (MFA) (Italy) Italy
  • Automatic Mirror Furnace (AMF) (Germany) Germany
  • Surface Forces Adhesion Instrument (SFA) (Italy) Italy
  • High Precision Thermostat Instrument (HPT) (Germany) Germany
  • Solar Constant and Variability Instrument (SOVA) (Belgium) Belgium
  • Solar Spectrum Instrument (SOSP) (France) France
  • Occultation Radiometer Instrument (ORI) (Belgium) Belgium
  • Wide Angle Telescope for Cosmic Hard X-rays (WATCH) (Denmark) Denmark
  • Timeband Capture Cell Experiment (TICCE) (Great Britain) United Kingdom
  • Radio Frequency Ionization Thruster Assembly (RITA) (Germany) Germany
  • Inter-Orbit Communications (IOC) (France/the Netherlands) France Netherlands
  • Advanced Solar Gallium Arsenide Array (ASGA) (Italy) Italy

The WATCH instrument observed Cosmic X-rays in an extremely wide field of view, a 65 degree range capable of observing 1/4 of the sky.[6] The design is a Rotation Modulation Collimator, in which stripes of NaI(Tl) and CsI(Na) detectors make a phoswich.[7]

Results

WATCH monitored about 25 X-rays sources over the whole sky over the course of the mission, as well as detecting 19 cosmic gamma ray bursts.[8] Many of the gamma ray bursts were able to be localized to within 1 degree.[9]

In the summer of 2016, EURECA was transported to the Swiss Federal Laboratories for Materials Science and Technology (Empa) in Dübendorf near Zurich where X-ray scans of the satellite were taken. The goal was to find out how EURECA's 11-month exposure to space had affected its structure and selected experiments it carried.[10] EURECA was then brought back to the Swiss Museum of Transport in Lucerne and has since been exhibited in a new way, with both solar panels fully deployed for the first time.[11]

See also

References

  1. ^ "NASA - NSSDCA - Spacecraft - Trajectory Details". nssdc.gsfc.nasa.gov. Archived from the original on 2019-07-26. Retrieved 2018-05-01.
  2. ^ "Archived copy" (PDF). Archived from the original (PDF) on 2007-09-30. Retrieved 2011-04-12.CS1 maint: archived copy as title (link)
  3. ^ "From Space to Lucerne". Eureca - a satellite on the road (again)! (YouTube channel). Archived from the original on 19 May 2020. Retrieved 5 June 2017.
  4. ^ EURECA Scientific Results, Advances in Space Research, Vol. 16, Issue 8 (1995) 1-140.
  5. ^ "Archived copy". Archived from the original on 2020-10-18. Retrieved 2020-11-09.CS1 maint: archived copy as title (link)
  6. ^ "The European Retrievable Carrier (EURECA) mission". heasarc.gsfc.nasa.gov. Archived from the original on 2019-07-26. Retrieved 2018-07-23.
  7. ^ "The European Retrievable Carrier (EURECA) mission". heasarc.gsfc.nasa.gov. Archived from the original on 2019-07-26. Retrieved 2018-07-23.
  8. ^ "The European Retrievable Carrier (EURECA) mission". heasarc.gsfc.nasa.gov. Archived from the original on 2019-07-26. Retrieved 2018-07-23.
  9. ^ "The European Retrievable Carrier (EURECA) mission". heasarc.gsfc.nasa.gov. Archived from the original on 2019-07-26. Retrieved 2018-07-23.
  10. ^ "Eureca X-Ray Scan". Eureca - a satellite on the road (again)! (YouTube channel). Archived from the original on 22 April 2020. Retrieved 5 June 2017.
  11. ^ "EURECA's last journey to Empa and back to Lucerne". Eureca - a satellite on the road (again)! (YouTube channel). Archived from the original on 23 April 2020. Retrieved 5 June 2017.

External links

This page was last edited on 8 January 2021, at 15:21
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