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Eureca

Spacecraft · Europe

Original archive entry. The text, images and links below are kept as they were written.

Eureca-1
Eureca-1
Credit: Manufacturer Image

European materials science satellite. Microgravity experiments; deployed from one shuttle mission, left in earth orbit for extended periods, and retrieved and returned to earth on a later shuttle flight. retrievable satellite satellite built by MBB-ERNO (prime) for ESA, Europe. Launched 1992.

Frequency plan: 2053.4583/22 30 MHz, 28 GHz/ 18 GHz (data-relay via Olympus).

More at: Eureca.

Country
Europe
Launch Vehicles
Space Shuttle
Agency
NASA
Bibliography
2, 279, 6

Chronology

1 event

1992 July 31

13:56 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39B. Launch Platform: MLP1. LV Family: Shuttle. Launch Vehicle: Space Shuttle.
  • Eureca-1 - . Payload: Atlantis F12 / Eureca 1 / TSS 1. Mass: 4,491 kg (9,900 lb). Nation: Europe. Agency: ESA. Class: Materials. Type: Materials science satellite. Spacecraft: Eureca. Decay Date: 1993-07-01 . USAF Sat Cat: 22065 . COSPAR: 1992-049B. Apogee: 509 km (316 mi). Perigee: 484 km (300 mi). Inclination: 28.50 deg. Period: 94.60 min.

    Microgravity experiments; deployed from STS-46 8/2/92; retrieved by STS-57; European Retrievable Carrier. EURECA is a European scientific and technology mission, launched by the US Space Transportation System. The spacecraft is scheduled to be retrieved likewise by the US/STS in late spring/early summer 1993. Designator ESA/92/01. Frequency plan: 2053.4583/22 30 MHz, 28 GHz/ 18 GHz (data-relay via Olympus).