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Far Ultraviolet Spectroscopic Explorer

Far Ultraviolet Spectroscopic Explorer
FUSE prelaunch crop.jpg
FUSE in a pre-launch cleanroom
Names Explorer 77
MIDEX-0
Mission type Ultraviolet astronomy
Operator NASA / JHUAPL
COSPAR ID 1999-035A
SATCAT no. 25791
Website http://fuse.pha.jhu.edu/
Mission duration Planned: 3 years
Final: 8 years, 3 months, 23 days
Spacecraft properties
Manufacturer Orbital Sciences / JHUAPL
Launch mass 1,360 kg (3,000 lb)
Dimensions 5.3 × 1.9 m (17.4 × 6.2 ft)
Power Average: 520 watts
Peak: 645 watts
Start of mission
Launch date 24 June 1999, 15:44 (1999-06-24UTC15:44) UTC
Rocket Delta II 7320-10
Launch site Cape Canaveral AFS SLC-17A
End of mission
Disposal Decommissioned
Deactivated 18 October 2007 (2007-10-19)
Orbital parameters
Reference system Geocentric
Regime Low Earth
Semi-major axis 7,127.8 km (4,429.0 mi)
Eccentricity 0.0010062
Perigee 742.5 km (461.4 mi)
Apogee 756.8 km (470.3 mi)
Inclination 24.9836°
Period 99.8 minutes
RAAN 129.8201°
Argument of perigee 246.2689°
Mean anomaly 113.6763°
Mean motion 14.43 rev/day
Epoch 18 April 2016, 11:52:03 UTC
Main
Wavelengths 90.5 to 119.5 nm (far ultraviolet)
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The Far Ultraviolet Spectroscopic Explorer (FUSE) is a space-based telescope operated by the Johns Hopkins University Applied Physics Laboratory. FUSE was launched on a Delta II rocket on 24 June 1999, as a part of NASA's Origins program. FUSE detected light in the far ultraviolet portion of the electromagnetic spectrum, between 90.5-119.5 nanometres, which is mostly unobservable by other telescopes. Its primary mission was to characterize universal deuterium in an effort to learn about the stellar processing times of deuterium left over from the Big Bang. FUSE resides in a low Earth orbit, approximately 760 km (410 nmi) in altitude, with an inclination of 25 degrees and just less than a 100-minute orbital period. Its Explorer designation is Explorer 77.

On 12 July 2007, FUSE's final reaction wheel, which is required for accurately pointing a spacecraft, failed and efforts to restart it were unsuccessful. An announcement was made on 6 September that because the fine control needed to perform its mission had been lost, the FUSE mission would be terminated.

Although the original specification was to have a Wolter-type grazing incidence telescope, the final design of the FUSE telescope comprises four individual mirrors. Each of the four mirrors is a 39-by-35 cm (15.4-by-13.8 in) off-axis parabola. Two mirror segments are coated with silicon carbide for reflectivity at the shortest ultraviolet wavelengths, and two mirror segments are coated with lithium fluoride over aluminum that reflects better at longer wavelengths. This optimizes performance over the entire spectral range.


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