Skip Navigation: Avoid going through Home page links and jump straight to content
NASA Logo - Jet Propulsion Laboratory    + View the NASA Portal
Search Stardust  
JPL Home Earth Solar System Stars & Galaxies Technology
Stardust Banner
Overview Mission Science Technology Newsroom Education Gallery Links Stardust Home
Weekly Status
Press Releases
Press Kits
Stardust in the News
Team Biographies
Media Contacts

STARDUST Status Report

February 25, 2000

There were five Deep Space Network (DSN) tracking passes during the past week. Commands were sent to the spacecraft to set the Command Loss Timer back to its original value of nine days. The spacecraft, due to interference from the Sun (solar conjunction), did not receive these commands last week, and they were retransmitted. Other commands were transmitted to the spacecraft to update the Small Forces, Earth ephemeris and Sun ephemeris files. These files contained updated information due to the trajectory and mass properties changes from the Deep Space Maneuver in January. All subsystems onboard the spacecraft are performing normally.

The spacecraft transitioned back to Gyro Based Attitude Mode with the Inertial Measurement Unit (IMU) powered on to provide high rate attitude data during the aerogel grid deployment. Also, six images were taken with the Star Camera. These images will be analyzed to determine the health of the Star Camera and provide information concerning why the number of valid stars occasionally drops from 10 to 4 stars.

A historic milestone in planetary exploration was achieved by STARDUST this week. The aerogel collector was successfully deployed to begin its interstellar dust collection. The commanded timeline was followed precisely with the heat shield on the Sample Return Capsule (SRC) opening, followed by the shoulder motor moving the collector out of the SRC and then finally the wrist motor extending the collector fully to its collection position where it sticks above the spacecraft dust shielding and into the interstellar dust stream.

The deployment was confirmed during deployment with small torques detected by the attitude control system as well as the motors turning for the proper time duration. The final confirmation came with the shoulder and wrist microswitches being triggered when deployment was complete.

In the spacecraft's current orbit, where it just came out of solar conjuction, its inertial velocity direction is about 49 degrees away from traveling directly with the interstellar dust stream. Over the next few months, as the spacecraft orbit curves around the sun, the spacecraft motion will parallel the dust stream motion.

After the collector was fully deployed and all subsystems were verified to be operating normally, a command was sent to move the collector 49 degrees in the direction of closing to position the collector surface area normal to the interstellar dust stream flow. Every few weeks the wrist motor will be commanded to change this angle by a few degrees to keep the collector surface normal to the stream. Near the end of this first interstellar collection period, the collector will be fully deployed again. This historic collection will continue until May 25, 2000; however, we are currently exploring extending this period by a few additional weeks.

There are no microswitches in between the full open and full close shoulder and wrist positions to tell us the exact position of the aerogel collector. Control and knowledge of this position during the next few months is achieved by commanding the wrist motor for a fixed length of time to provide the desired angle movement and then verify this movement from telemetered wrist motor operating data. To reach its current 49 degree offset angle, the wrist motor was powered on for about 20 seconds, which was executed perfectly.

The collector has two sides of aerogel: side A for interstellar dust collection and side B for cometary dust collection. We control which side of the collector is exposed to a dust stream by orienting the side of the collector is exposed to a dust stream by orienting the spacecraft in inertial space. Currently the spacecraft is oriented with its dust shields pointing in the direction of its motion about the sun and the interstellar dust particles hitting the back side (side A) of the collector. The spacecraft orientation with be reversed relative to the Comet Wild 2 particle stream so that the dust shields will protect the spacecraft while the collector is extended above these shields, into the oncoming dust stream.

As its name indicates, the interstellar particles to be collected now are from outside of our solar system. There is a very tenuous dust cloud within our galaxy, the Milky Way, which our solar system is moving through. The direction of the interstellar dust is opposite to the motion of the sun, which drags the planets with it, relative to the particle media. Thus, the dust motion is small relative to the solar system motion that is controlling the direction of interstellar dust passing through our solar system.

The interstellar dust stream was detected many years ago by earth orbiting spacecraft and earlier Pioneer and Voyager spacecraft have improved information on this stream. More recently, the Ulysses and Galileo spacecraft have confirmed the stream direction as well as indicated that the density of particles in the stream is very low.=20 With the size of the STARDUST collector being only about 0.1 meter square, on the order of 100 such particles are expected to be collected during the 2 collection periods. The second collection period is in about two years, when again the spacecraft is traveling in the direction of the particle stream.

High praise goes to the spacecraft builder and flight operations team at Lockheed Martin Astronautics in Denver, Colorado for this successful deployment and the start of the sample collection. The interstellar particles will be returned to earth with the Wild 2 particles for detailed scientific analyses in 2006, after the SRC lands in the Utah Test and Training Range.

Following the successful deployment, three images were taken with the Navigation Camera. These images were taken through the Optical Navigation filter (widest bandwidth) with the calibration lamp on. Two images had an exposure time of 200 milliseconds and the third had an exposure duration of 1 second. These images will be analyzed to help determine the cause of the apparent decrease in Navigation Camera sensitivity observed when the last star images were taken in October.

Also, after the aerogel collector deployment, the spacecraft transitioned back to All Stellar attitude mode.

For more information on the STARDUST mission - the first ever comet sample return mission - please visit the STARDUST home page:

Last Updated: November 26, 2003
Privacy F.A.Q. Contact Sitemap Credit
FIRST GOV + Freedom of Information Act
+ The President's Management Agenda
+ FY 2002 Agency Performance and accountability report
+ NASA Privacy Statement, Disclaimer, and Accessiblity Certification
+ Freedom to Manage
NASA Home Page Site Manager:
Aimee Whalen

Ron Baalke