2002
Genesis Mission Status Updates: April, May, June
June 27, 2002
We continue to remain in low-speed solar wind. The concentrator
rejection grid autorecovery patch was uploaded on Monday,
which was over a week earlier than planned. At the same
time, the rejection grid's maximum voltage was raised
to 2060 V. The team estimates that approximately 1350
commands have been radiated to the spacecraft since
launch. Genesis has been collecting solar wind particles
for almost 7 months now.
June 20, 2002
We've had a lot of low speed solar wind over the last
week; everything's normal.
A regularly scheduled test of the solar wind concentrator
rejection grid was conducted on 6/17, and set a record
high of 2100 Volts (up from 2080 Volts). The concentrator
was returned to autonomous mode at the end of the test.
While the results were encouraging, the science team
did not deem the improvement large enough to alter the
autonomous mode's operating configuration.
June 14, 2002
It's been a quiet week in space. The spacecraft continues
to collect solar wind samples. Genesis has been collecting
solar wind samples for 179 days and is scheduled to
continue. The solar wind Genesis has observed has been
in the low-speed regime. In two weeks, the Genesis spacecraft
will be its farthest distance from the Sun this year.
June 6, 2002
The spacecraft continues to collect solar wind samples.
Coronal mass ejections, fast solar wind/coronal holes,
and slow solar wind regimes were all observed and the
appropriate arrays were deployed to collect samples
from each type of solar wind.
The navigation team issued the final reconstruction
report on station keeping maneuver 2A, which was done
on May 22. The total change achieved (0.7926 meters
per second) was just 0.09 percent less than the change
planned.
A 1-hour diagnostic test was performed this week on
the Genesis ion monitor. Los Alamos National Laboratory,
which supplied the monitor, will analyze the data.
May 30, 2002
The Day the Solar Wind Disappeared:
Genesis continues to collect solar wind samples. The
solar wind exhibited some unique behavior over the last
week, including a "day when the solar wind disappeared."
The spacecraft detected extremely low densities (one
particle in ten cubic centimeters or less than one particle
in a cubic inch), extremely high wind speeds (approaching
1000 kilometers per second, or over 2,000,000 miles
per hour), and multiple coronal mass ejections.
The onboard WIND algorithm was stumped by this rare
behavior, so it positioned the collector arrays to a
conservative configuration and set the concentrator
high voltages to zero until conditions became more normal.
More recently, WIND has detected a more normal coronal
mass ejection regime and the arrays and concentrator
have responded as intended.
We continue to have indications that last week's station-keeping
maneuver was very accurate and maybe the best yet.
May 16, 2002
Genesis has now successfully completed the first of
its five planned loops. Preparations are well underway
for the next station-keeping maneuver (SKM), scheduled
for May 22nd. The solar wind has been mostly low speed
over the last week.
The flight software team has begun to work on a patch
that will automatically reset the concentrator rejection
grid voltage, rather than turn the concentrator off,
if a latch-up occurs.
Telecom is nominal. We are currently downlinking data
from the spacecraft at a rate of 47,400 bits per second
and uplinking commands to the spacecraft at 2000 bits
per second. Although there may be some variation in
the signal, there will be no telecom configuration changes
for the upcoming station-keeping maneuver.
May 9, 2002
It's been a quiet week; science collection continues
as planned and all systems are operating well. The seventeenth
background sequence went active on May 7th. The next
stationkeeping maneuver (SKM-2A) should take place May
22nd and will be about 0.8 meters per second change,
about 21 degrees off-sun.
It takes about 11 seconds for a signal to leave Earth,
go to the spacecraft and come back.
The solar wind has been mostly low speed over the last
week.
April 25, 2002
On Sunday, the second strongest solar storm since launch
passed over the spacecraft: high-energy protons at a
level several orders of magnitude higher than normal
bombarded the spacecraft. Due to previous improvements
in the onboard software, the spacecraft weathered this
well.
During the solar storm, the star tracker lost track
four times. The Attitude Control software handled the
situation as intended so that overall spacecraft performance
was unaffected and all daily maneuvers were completed
as scheduled.
A Deep Space Network pass on Friday, April 19, revealed
that a minor lapse in the solar wind concentrator occurred
at 19:36 UTC on Wednesday, April 17, when the actual
rejection grid voltage did not match the requested voltage.
Either the solar environment or a random high-voltage
arc in the rejection grid could have caused the fault.
After the science team analyzed it, the concentrator
was turned back on and the rejection grid was tested.
The concentrator performed exactly as it had earlier
this month before the solar storm. Following the test,
the concentrator was configured for a slightly lower
rejection grid limit voltage and put back in autonomous
mode.
April 18, 2002
For the Genesis spacecraft, solar particle collection
continues as planned. The propulsion system is normal;
a total of 13.14 kg of fuel has been used since the
start of the mission.
The team has begun work on the next spacecraft background
sequences containing flight software diagnostics, data
management, clock correlation commands, daily precessions,
ion and electron monitor calibrations, and collector
array management surrounding the daily precessions.
The sequence will cover 28 days and will be sent to
the spacecraft on May 3.
On May 22, Genesis will conduct its fourth station-keeping
maneuver, which ensures that the spacecraft maintains
its orbit around the Lagrange point.
April 11, 2002
This past week, Genesis detected and low speed solar
wind, high-speed solar wind/coronal hole, and a borderline
coronal mass ejection.
A total of 13.13 kg of fuel has been used since the
start of the mission, and 1.84 kg since the start of
science.
Telecom continues to report good performance. The spacecraft,
using the 26-meter Deep Space Network dish in Canberra,
Australia, identified a ground station setting change
that boosted performance.
April 4, 2002
The concentrator rejection grid patch was uploaded last
Friday and is working normally. Just hours after the
upload, the rejection grid properly went to 1880 volts
when it detected some very high-speed solar wind, with
speeds up to ~800 kilometers per second (2 million miles
per hour.) On April 3, we performed another concentrator
rejection grid test. Repeatable performance of the rejection
grid was achieved up to 2080 volts, showing that the
grid has "healed" by ~200 volts since January.
The navigation team completed its reconstruction of
station keeping maneuver 1C and reports excellent performance. |