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INTERVIEW WITH FLORENCE TAN

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Hi, my name is Florence Tan.  I’m an electrical engineer at Goddard Space Flight Center.  I have built and am building electronics for mass spectrometers flying in space.  I have built electronics on mass spectrometers that are flying on the Cassini Mission.  One (the mission) now orbiting Saturn. 

I’m here to talk about the sun’s affects on spacecraft flight instrumentation.  The sun provides a headache for me in terms of design for space.  I have to mitigate for the affects of the sun when I design for space.  The affects are radiation and heat.  The radiation can be particles or ionizing radiation.  These particles and radiation vary with the conditions of the sun.  If you have an active sun you have an active environment for charged particles and radiation goes up.  Higher energy radiation such as x-rays and gamma rays can damage packaged and integrated circuits, crew and internal parts, similarly with the particles.

We all use a radiation unit called a rad to measure the affects of radiation.  For example on Cassini I used parts that can withstand 100,000 rads, 100 kilo rads.  For comparison medical fluoroscopy or x-rays have .4-4 rads.  200 rads causes a person to be sick and 600 rads is fatal in 90% of the cases in 1-2 weeks and 10,000 rads is instant death.

So, what does radiation and particles do to the material?  The radiation and particles can cause things called “latch out” which physically damages the integrated circuit to the point that it’s stuck on zero or one bit.  It damages the structure which damages the structure of the electrons.  Another thing it does is it can change a zero to one and one to zero and that also causes problems because the program has changed. 

In addition charged particles can cause a phenomena called spacecraft charging.  This is when the spacecraft environment is charged in a geomagnetic storm where the spacecraft

Is charged and what you’ll have is differential charging from one part of the spacecraft to the other.  Eventually electrical charges can arc across spacecraft components in harming and possibly disabling them.  All of these are radiation and particle effects 

There are many ways to mitigate this.  One way to mitigate is to use shielding with a denser material like aluminum or lead.  And the other thing we’ve done is to use parts that are naturally immune to these affects called single event affects.

Now, about heat.  The heat of the sun causes the atmosphere around the earth to expand up to 1000 kilometers.  So, what happens to a spacecraft orbiting the sun is that the sun…  When it expands it cause drag on the spacecraft and the spacecraft will have to continually boost its orbit.  That happened to Skylab and we have premature mission death or end of the mission.  The other thing with thermal cycling is when you have fatigue to the materials.  So careful thermal design is extremely important when you design for space.  So, in conclusion we have radiation and particles thermal affects that we have to design for.  If you’d like to learn more about this subject please visit the website and have fun.  Thank you.

 

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Last Updated: April 28, 2008