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| subject: | 1\24 Japan-MUSES-C Microwave Ion Engine Prototype Reaches 18000 |
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Microwave ion engine prototype model achieved 18000 hrs of autonomous
endurance running!
ISAS, Japan
January 24, 2003
The spacecraft for asteroid sample return mission, MUSES-C, scheduled
for launch in May 2003, will have an ISAS-developed microwave ion
engine onboard for interplanetary navigation. The prototype model of
this engine has achieved 18000 hours of autonomous endurance running.
The ion engine that started the endurance test on March 30, 2000 to
verify its performance for the mission requirement of 18000 hours has
continued autonomous running over approx. 2 and a half years. It
successfully achieved the original goal of 18000 hours at 2:00AM on
October 25, 2002, and still keeps running at present. The engine used
for the endurance test is a prototype model of MUSES-C and has been
produced in complete accordance with the design, material and
manufacturing of the flight model.
[Image]
Figure: Cumulative running hours and screen current over calendar time
The figure shows the cumulative time (graduations on the left) from
the start of the test up to the achieving point of 18000 hours and the
screen current corresponding to thrust (graduations on the right) over
calendar time. As shown in the figure, there are some breaks in the
sequence of cumulative time. They indicate the engine cutoff due to
the following reasons and do not indicate in any way malfunctioning of
the engine: use of endurance test facilities for flight model testing
and adjusting; legally scheduled power cut and regular maintenance and
inspection of the engine; troubles in the ground support equipment
such as a cooling system. Moreover, through the entire test period,
the engine has successfully maintained the required thrust performance
level, which clearly proves its high potential as a reliable engine in
the future.
[Image]
Picture: Running ion engine
The picture shows the running engine after it has achieved the target
18000 hours. Xenon is used as the propellant, and electrons are
emitted from the luminescent point, neutralizer, in front. Some wear
due to Xenon sputtering shown around the ion beam acceleration and
outlet areas is well within expectation and has no impact on the
performance of the engine.
http://www.isas.ac.jp/e/new/release/2002/12_04.html
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