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Explorer: FUSE (MIDEX 0)

FUSE [OSC]

FUSE (Far Ultraviolet Spectroscopic Explorer) represented the next generation, high-orbit, ultraviolet space observatory covering the wavelength range of 90.5-119.5 nm. The primary objective of FUSE was to use high-resolution spectroscopy at far ultraviolet wavelengths to study the origin and evolution of the lightest elements (hydrogen and deuterium) created shortly after the Big Bang, and the forces and processes involved in the evolution of galaxies, stars and planetary systems.

The spacecraft was launched as a joint US-Canada-France project. Only one previous mission, Copernicus, has given us this far-ultraviolet region of the electromagnetic spectrum. However, FUSE will provide a sensitivity some ten thousand times greater than Copernicus.

The FUSE satellite consists of two primary sections, the spacecraft and the science instrument. The spacecraft contains all of the elements necessary for powering and pointing the satellite, including the Attitude Control System, the solar panels, and communications electronics and antennas. The science instrument includes the telescope mirrors, the spectrograph (and its detectors), and an electronic guide camera called the Fine Error Sensor (or FES). The spacecraft and the science instrument each have their own computers, which talk to each other to coordinate the activities of the satellite.

FUSE was planned as a grazing incidence Wolter-Schwartzschild Type II telescope with an aperture of 80 cm, feeding an array of sensitive far-UV and EUV (wavelength 90.5 - 118.5 nm) spectrographs equipped with Photon Counting Array (PCA) detectors. The FUSE observatory was designed for an operational lifetime of three years, although it is hoped that it may remain operational for as long as ten years.

The observatory is approximately 7.6 m long with a baffle fully deployed. S-band transponders of 5 W output capacity will allow transmission of the scientific data at a rate of 40 kbps. A complete image may be read out in about seven minutes. Spacecraft housekeeping data, and compressed data will be downlinked at 2 kbps.

Nation: USA
Type / Application: Astronomy, Far-UV spectroscopy
Operator: NASA
Contractors: Orbital Sciences Corporation (OSC) (Bus), Johns Hopkins University Applied Physics Laboratory (APL) (Instrument)
Equipment: FUV telescope and spectrometer, FES
Configuration: MidStar
Propulsion:
Power: 2 deployable solar arrays, batteries
Lifetime: 3 years
Mass: 1334 kg
Orbit: 753 km × 769 km, 25.0
Satellite COSPAR Date LS Launch Vehicle Remarks
FUSE (MIDEX 0, Explorer 77) 1999-035A 24.06.1999 CC SLC-17A Delta-7320-10C

References:

  • NSSDC Master Catalog: FUSE
  • Orbital Sciences Corp.: FUSE