Small Explorer / WIRE
SMEX / WIRE
|Mission type||Infrared astronomy|
|Operator||NASA / GSFC|
Bowie State University (BSOCC)
|Mission duration||4 months (planned)|
1y, 4m, 10d (achieved) 
|Manufacturer||Space Dynamics Laboratory (SDL)|
|Launch mass||250 kg (550 lb)|
|Start of mission|
|Launch date||5 March 1999, 02:56 UTC|
|Launch site||Stargazer, Vandenberg Air Force Base|
|Contractor||Orbital Sciences Corporation (OSC)|
|Entered service||Failed on orbit|
|End of mission|
|Deactivated||30 September 2000|
|Decay date||10 May 2011, 07:00 UTC|
|Reference system||Geocentric orbit|
|Perigee altitude||470 km (290 mi)|
|Apogee altitude||540 km (340 mi)|
|Diameter||30 cm (12 in)|
The Wide Field Infrared Explorer (WIRE) was a satellite launched on 5 March 1999, on the Pegasus XL rocket into polar orbit between 409 and 426 km (254 and 265 mi) above the Earth's surface. WIRE was intended to be a four-month infrared survey of the entire sky at 21-27 µm and 9-15 µm, specifically focusing on starburst galaxies and luminous protogalaxies.
The science team was based at the Infrared Processing and Analysis Center (IPAC) in Pasadena, California. Flight operations, integration, and testing were from Goddard Space Flight Center in Maryland. The telescope was built by Space Dynamics Laboratory in Utah. Premature ejection of the spacecraft aperture cover led to depletion of the solid hydrogen shortly after launch, ending the primary science mission. The onboard star tracker remained functional, and was used for long-term precision photometric monitoring of bright stars in support of an asteroseismology program. WIRE reentered atmosphere of Earth on 10 May 2011 (around 07:00 UTC).
The Wide-field Infrared Explorer (WIRE) was a two-color, solid hydrogen-cooled, infrared imaging telescope designed to study starburst galaxies and to search for protogalaxies. The science goals of WIRE were to: 1) determine what fraction of the luminosity of the universe at a redshift of >0.5 is due to starburst galaxies; 2) assess how fast and in what ways starburst galaxies evolve; and, 3) examine whether luminous protogalaxies are common at redshifts <3. In order to accomplish these goals, WIRE was to conduct a four month survey at 12 and 25 µm over an area of between ten and several hundred square degrees of the sky.
The WIRE telescope itself had an entrance aperture of 30 cm and a 32 x 32 arc-minute field of view. It was of a Ritchey–Chrétien telescope design with no moving parts and no reimaging optics. Shortly after launch, while the spacecraft was still tumbling early after orbit insertion, the telescope cover came off prematurely. This resulted in the exposure of the cryogenic materials to light, warming them at a high rate causing outgassing and increasing the rate of spin of the spacecraft beyond the ability of the reaction wheels to slow it. Although ground controllers began work to decrease the excess spin of the spacecraft, they were not able to do so in time to prevent the total loss of the frozen hydrogen used to cool the primary science instrument. Attempts to recover control of the spacecraft were successful, though as a result of the coolant loss no science data were obtainable.
A design flaw in the spacecraft control electronics caused the telescope dust cover to eject prematurely in its first few hours on-orbit, exposing the telescope to the Earth. In normal operations, the telescope would avoid pointing at the Earth as well as the Sun because the heat load was too high for the cryogenic cooling. At this early stage in the mission, the telescope was deliberately pointed at the Earth for safety under the assumption that the dust cover was present. The influx of power into the telescope caused the solid hydrogen cryostat to boil off all of its cryogen. The cryostat was designed to non-propulsively vent small amounts of gaseous hydrogen as the instruments were cooled. However, due to the unexpected heating, the vent began expelling gas at rates orders of magnitude higher than designed. The over-active vent acted as an uncontrolled, off-axis thruster. Eventually, the attitude control system was unable to counter the thrust of the cryostat vent, and the spacecraft began to spin. By the time the hydrogen supply was exhausted, the spacecraft was spinning as fast as 60 rpm. As the thrust finally abated, spacecraft engineers were able to re-establish attitude control. However, with the cryogen gone, the science instrument was no longer functional and the original science mission ended.
In order to salvage some functionality from the US$73 million spacecraft, operations were redirected after the failure of the cryogenic system to an alternate science mission using the undamaged onboard star tracker for long-term monitoring of bright stars in support of an asteroseismology program. This technique aims to measure oscillations in nearby stars to probe their structure. While the star tracker has poor spatial resolution, having been designed primarily for a wide field of view and detection of the brightest stars, it is above the atmosphere and thus avoids scintillation, enabling high-precision photometry. As a secondary experiment, one solar array includes a section with reflectors, to test a concentrator system.
The original science goals of WIRE may finally be achieved by the Wide-field Infrared Survey Explorer (WISE) mission which was successfully launched into orbit on 14 December 2009, and began observations on 14 January 2010.