The beginning of IUE goes back to the late 1960's and the success of the
early astronomical satellites such as OAO-2 and Copernicus (OAO-3) in
the US and TD-1 in Europe. Various studies were being pursued at NASA
and within the European Space Research Organization (ESRO, the
predecessor of ESA) for new astronomy satellites. One such study, for
an Ultraviolet Astronomical Satellite (UVAS), was proposed by a team
from the UK. This became the basis for a joint project among NASA,
ESRO, and the UK's Science Research Council (SRC).
The approval process was especially challenging, since it involved three
different agencies. But approval for the International Ultraviolet
Explorer was won in 1971. Under the interagency agreement, NASA was
reponsible for the overall system design, design and construction of the
telescope, spectrograph, and spacecraft, the launch, and the US
spacecraft control station at Goddard Space Flight Center (GSFC). The
UK was responsible for the design and construction of the cameras and
contributed to the optical design and the sunshade. ESA provided the
solar arrays and the European spacecraft control station near Madrid,
Spain.
Several unique design elements were part of the planned IUE mission.
First, the spacecraft was to be placed into geosynchronous orbit. This
would allow it to be controlled in real time and thus be operated much
like a ground-based observatory. Weight was therefore a major
consideration. One compromise was to place the spacecraft into an
eccentric orbit. In this orbit, the spacecraft dipped into the Van
Allen belts at perigee. This became the "US2" high radiation shift,
during which observers took shorter exposures because of the radiation
background affecting the cameras.
Second, the goal of a long scientific mission was incorporated into the
project design. The scientists pushed hard for a five-year mission. But
the engineers would agree only to a three-year design lifetime, with
a five-year "goal" as a compromise. Ironically IUE lasted much
longer than five years!
Finally, control of the satellite would be passed between two
control stations on two different continents. This concept caused some
concern, since a clear chain of command is required for safe, successful
spacecraft operations. Various steps were taken to insure
well-coordinated operations. A standard protocol was used for "handover"
of command between the two stations. The Goddard control center stayed
online during VILSPA shifts to monitor and backup the European
operations. Both stations used essentially identical command computers,
software, and Flight Operations Directives.
Concerns about the radiation enviroment resulted in the last-minute
installation of a radiation monitor. As it turned out, the radiation
environment was not as bad as feared, but the radiation monitor was very
useful in helping the observers better estimate exposure times during the
high radiation shift.
IUE was launched on January 26, 1978, on a Delta rocket from
Cape Canaveral, Florida. It was placed initially in an eccentric
transfer orbit, then the apogee boost motor was used to circularize the
orbit. After this IUE was so close to its nominal station (i.e.
longitude) that it was not neccesary to use the jets move the spacecraft
orbit. Initial check-out of the hardware went smoothly. The first
spectrum, of the calibration star Eta Ursae Majoris, was obtained on the
third day.
The spacecraft was then operated for 60 days under a Commissioning
Period. Various high priority calibration and science observations
were performed. For each spectrograph, there were prime and redundant
cameras. It was quickly learned that the Short-Wavelength
Redundant (SWR) camera was not functioning
properly, and it was not used after the Commissioning Period. The
SWP camera experienced significant microphonic noise, a major concern,
until the source of the noise was found (the Panoramic Attitude Sensor,
used for attitude determination after launch) and turned off. The LWP
camera, in some ways better than the LWR, experienced sporadic scan
errors, so the LWR was chosen as the default long-wavelength camera.
Routine operations began on April 1, 1978... and continued until
October 30, 1996, an amazing 18 years and 9 months!
More information?
Please see "The History of IUE"
(Boggess, A., Wilson, R., Barker, P. J., and Meredith, L. M. 1987, in
Scientific Accomplishments of the IUE, Reidel: Dordrecht, ed. Y.
Kondo, pg. 3). Most of the information above is condensed from this
excellent article.
In addition, please see the series of articles written about IUE
published in Nature , beginning with Boggess, A., et al.
, 1978, Nature , 275 , 372. The first
paper describes IUE, while the others describe the results of the
Commissioning Period observations of various types of astronomical
objects.