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U P D A T E # 1 4 PART 1: Galileo
fact of the day (see http://www.jpl.nasa.gov/galileo/fact for a complete list) A day on Jupiter is only 9 hours and 48 minutes long. Such fast rotation causes Jupiter to be somewhat squashed due to centrifugal force: its polar radius is 4000 km less than its equatorial radius (the latter being 71,392 km). That means you'd weigh almost 25% more at Jupiter's poles than at its equator, that is, if you could find a place to stand! So a 100 pound person (on Earth) would weigh 230 pounds at Jupiter's equator but 285 pounds at the pole! To recap, we suggest that after each Probe Squash installment, you and your students make a prediction about how long the Probe's mission will last. Installment #7: Battery lifetime: electricity is vital The Probe Battery: It Keeps Going, and Going, and Going..... Before the Probe was released, it was able to draw power from the Orbiter. Now that it's on its own, it relies on a battery. And not just any battery--the Probe's lithium/sulfur dioxide batteries have to stand up to conditions far tougher than anything that D cells from the supermarket are designed for. Once the Probe separated from the Orbiter, the batteries provided the only power source for the Probe during its almost 5 month long journey to Jupiter. (A side note--one of the things that the Probe engineers had to be very careful about while getting ready for Probe separation from the Orbiter was to make sure that the batteries weren't accidentally discharged!) Therefore, it was important to conserve energy on board the Probe, so everything was turned off, with the exception of a timer that would "wake" the probe six hours before entering the atmosphere. If the battery ends up running down faster than expected, the Probe mission can't last as long. But we won't know the battery's status until the Probe wakes back up. When they're not being used (when they're not "under load"), the lithium batteries have a voltage of 39 volts. Fresh out of the factory, they have a total capacity of 21 ampere hours (an "ampere hour" is enough electricity to keep a one ampere current flowing in a circuit for an hour), of which one ampere hour will be lost as the battery ages (the battery, after all, is over six years old!); during the descent portion of the mission, an ampere-hour of energy is used every 7 minutes). The Probe mission calls for the battery to function for an hour after the Probe enters the atmosphere; by that time, the Probe should use up about 18 ampere hours. With the remaining two ampere hour margin, there should be enough power to last for at least 75 minutes after Probe entry, assuming that the Probe powers up no earlier than scheduled. (There are other batteries on board as well--two thermal batteries are used for pyrotechnic events. You can hear the thermal batteries igniting, and smell them after they ignite! Specifically, thermal batteries are used for 1) the mortar fire that will send out the pilot parachute, 2) the release of the Probe heat shields, 3) extending the Nephelometer (or cloud sensor) arm, and 4) activating the sharp cable cutters that will sever wires connecting the Probe's outer protective shell to its inner capsule.) To test the battery, a spare battery that was built at the same time as the flight one (and therefore is just as old), and has been kept at the same temperature as the flight battery, was hooked up to run under similar loads and temperature. The loads are more severe than the actual Probe battery will face. The test was run using the higher loads because this had been the estimated load that, years earlier, before the exact loads on the spacecraft were known, engineers had predicted the battery would face. To make it easier to analyze the test results, the testing conditions weren't changed from test to test over the entire lengthy history of the program. Under this test, the battery lasted 68.5 minutes. After adjusting for the fact that 1) the flight battery will experience smaller loads, and 2) the flight battery will be some ten months older when called upon to do its job than was the battery used in the test, Probe engineers are predicting that the battery will be able to keep the Probe powered for 75.7 minutes. That will take the Probe down to almost 30 bars of pressure, or about 193 degrees Celsius. Do you regard this as good news or bad news for the Probe's total lifetime? And, something to think about for next time: so far, we've talked about how to keep the Probe "alive." But how do we get the Probe's data from the hostile Jovian environment back to Earth? Robert B Gounley 1989 would be the big year for my project -- the year the Galileo spacecraft would be launched. Even before launch, many years and hundreds of careers had already been invested in the mission. By mid- October, with launch imminent, most of the flight team members were visibly excited. Old-timers like me (by then, seven years on the project) were more introspective; we had been here before. When the project was approved in 1977, plans called for a 1982 Space Shuttle launch along with a large booster rocket (its upper stage) to send Galileo off to Jupiter. Within a few years, delays in the Shuttle program forced Galileo's launch to "slip" to 1984. Later, funding problems with the upper stage forced a further delay, until 1985. In between, each new federal budget seemed to threaten Galileo with outright cancellation and each time Galileo managed to hold on. The engineers and scientists working on Galileo, all coping with formidable technical challenges made more complicated by each change to the mission, held on as well, hoping each postponement would be the last. When I joined Galileo in December 1982, launch had just slipped to May 1986. This seemed more secure than previous dates. By now, the Shuttle had launched five times and funding for our upper-stage, the Shuttle- Centaur, was firmly in place. Morale picked up as we began to assemble and test the largest and most complex planetary explorer ever. In 1984, a milestone had been reached -- two years until launch. We had never been that close before! By January 1986, I was spending most of my waking hours at work, preparing for Galileo's launch. Testing was complete and the spacecraft had been shipped by flat-bed truck from JPL in Pasadena to the Kennedy Space Center, where it become space shuttle Atlantis's prime cargo. Now, among other duties, I was the systems engineer responsible for the first maneuver Galileo would perform. This called for firing the spacecraft's thrusters about 10 days after launch to assure that its course would take it on a fly-by of the asteroid Amphitrite along the way to Jupiter. After years of designing, testing, and trouble-shooting Galileo, I was on the team that would fly it. Unfortunately, there was no owner's manual in the glove compartment. Early on morning of January 28, 1986, the Galileo flight team assembled in a large conference room for another in a long series of training lectures. Some of us rubbed sleep from our eyes while others fidgeted, thinking of the work remaining back at our desks. Overhead, the TV monitors were all tuned to NASA's internal television network. Later that day, there would be a press conference announcing Voyager 2's discoveries at the planet Uranus. Meanwhile, the monitors showed preparations to launch another Space Shuttle. For us, that launch meant that there would be only one more to go before our own. The lecture crept along, broken by many questions and clarifications. Finally, someone suggested we take a short break to watch the shuttle launch. We all looked up in time to watch the Space Shuttle Challenger liftoff and clear the tower. Since the TV monitors had their sound off, people chatted freely. Over my shoulder, someone said, "It's amazing how that thing works every time." On the screen above, Challenger was fading into the sky. By now, we knew the shuttle launch sequence by heart. Soon the solid rocket motors would burn out and separate. We were all startled when we saw what appeared to be an early separation of the solid motors. As the seconds dragged, a growing fireball filled the screen, showing many pieces dropping from the sky. Without spoken commentary from the TV, no one knew for sure what was happening. In some launch failures, the shuttle can return to the launch site for a runway landing. Was Challenger on its way there now, out of sight of the TV camera? Someone said the monitors in the cafeteria next door might have sound. About a dozen of us bolted for the doors. The cafeteria monitors were silent also, but as we arrived, the NASA cameras had panned downward to watch large pieces of debris hit the ocean. There was no sign of Challenger gliding toward a runway. We all felt grief in our own ways. A few cried. Others stared vacantly at the screen, then slowly ambled away. The Astronaut Corps, the most visible side of NASA, came to represent the many thousands of us that worked in the space program. We lost family that day. On the Galileo project, our actions, which a short time earlier were energetic and purposeful, became lethargic and disjointed. Would Galileo ever launch? Would there be planetary exploration at all in the near future? Within a day, our Project Manager, John Casani, returned from Florida where he had been overseeing Galileo launch preparations. We assembled in the cafeteria and John spoke atop a chair so he could be seen and heard by everyone. He confirmed, as most had already assumed, that no one knew when to expect another shuttle flight. In the meantime, our work to prepare for launch and flight operations remained very important and we were all expected to continue. Galileo would launch someday and the knowledge required to fly it must be "captured" while this flight team remained together. Meanwhile, others would go off to plan a new mission 1986 dragged on with new options considered and dropped almost weekly. For a while, a 1987 launch seemed possible. Soon the new launch date moved to 1988 and finally settled at October 1989. Our upper stage-- the Shuttle-Centaur booster, which used cryogenic liquid fuel--had been canceled a few months earlier. The spacecraft was now going to use the much smaller Inertial Upper Stage (IUS) booster. To get to Jupiter, Galileo would have to take a six-year looping trajectory through the inner solar system rather than a two-year direct flight. More importantly, the spacecraft would have to be significantly modified to fly much closer to the Sun than the original flight path called for. The added time was a disappointment, but there was now so much more to be done. By October 1989, the spacecraft was inside the Space Shuttle Discovery, awaiting launch. A new flight team had been assembled, about an even mix of new faces and old. This time, I was in charge of early cruise activities to check out Galileo's operation -- a "shake-out" to uncover problems before the Venus fly-by next February when solar heating would be at its worst. Depending on the day Galileo launched, my command sequence would have to be adjusted (since the actual trajectory would be somewhat different from the planned trajectory). Unfortunately, that meant that during launch I would not be stationed in Galileo's Mission Support Area (the MSA being Galileo's version of Apollo 13's Mission Control - Houston). Rather, I would have to stay fresh to rework my commands soon after Galileo was sent on its way. This wasn't the happiest possible arrangement for me, but I accepted that responsibilities had to be divided and there were others who were more qualified to do the monitoring. Besides, the last thing the MSA needed were people standing around "just to be there" and obstructing other's concentration. In the weeks prior to launch, some friends and I conspired to make our own personal statement on Launch Day. This project consumed most of the precious personal time we had, but it seemed not to matter. How many times does someone get to celebrate the start of a planetary voyage? Galileo's launch date was set by the positions of the planets. For a proper gravity assist, the spacecraft must approach Venus at precisely the right time and in precisely the right direction and speed. Our upper-stage would deliver most of the energy required for this; the rest would come to launch and, on either side of it, days when you could get to Venus by using more fuel. In hard terms, this meant Galileo *had* to be launched sometime between October 12 and November 21, or the increased fuel cost would force us to delay launch until the next favorable planetary alignment six months later. To make matters worse, the Space Shuttle had its own constraints that determined what time of day it could launch. In the middle of our launch period we might have a "launch window" lasting over an hour, but near the beginning and end there would only be minutes to launch on each day. A streak of minor problems or one large one could keep Galileo earthbound until the following year. As our launch period began, everyone waited nervously as the shuttle prepared for launch. Minutes ticked away and then an announcement came from Florida. The shuttle had a problem with one of its computers and the launch that day was scrubbed. A week later, with the computer repaired, our countdown began again. This time, clouds rolled in over the launch site and weather forced another cancellation. October the 18th was a bright and sunny day in Pasadena. There were still clouds in Florida, so many of us expected that day's launch would be scrubbed also. Either that, or some other problem would cause a delay. Working on Galileo, we had learned to accept such things. Friends in the MSA that morning tell me that when the launch clock finally started ticking down to the single minutes, they looked at each other with eyes wide. They were really going to do it! In a conference room in another building, I watched a TV screen with a roomful of other Galileo personnel. There was a buzz of nervous chatter right up to the final seconds before launch. Al Hoffman, our chief environmental engineer, kept a watchful eye on the door to make sure latecomers had a view. When the Space Shuttle cleared the launch tower, the room erupted with cheers and applause. The noise subsided as the shuttle rose higher and we remembered another launch three and a half years earlier. We held our breaths as Discovery passed through one minute of flight and then two. Cheers rose up again when we saw the shuttle's solid-rocket motors burn out and fall safely away. Fists punched the air and hands slapped each other in "high-fives". Others slumped contentedly in their chairs, relieved that their wait was finally over. With the shuttle, and our spacecraft, safely on its way to Earth orbit, Al Hoffman began handing out lapel pins commemorating Galileo's launch. It was the first of many similar pins I would receive. My co-conspirators and I looked at each other. The shuttle, with Galileo aboard, was in space at last. This was the right time. We went to a utility closet and took the bundle of cloth, wood, and rope that we had worked nights and weekends to prepare. On the roof, we spread apart as planned and began to tie our rigging. Over the side we hung our banner measuring about 10 feet high by 50 feet wide, all in white with large blue lettering. "Galileo: WE'RE ON OUR WAY!", it said in print large enough to be plainly seen from JPL's plaza, eight stories below. Fluttering in the sun that clear fall morning, it was a beautiful sight. Perhaps it was an extravagant gesture, but it spoke of the pride and satisfaction felt that day. We wanted to tell the world about it. Whatever the future held, Galileo was earthbound no longer. --------------------------------------------------------------------------- Bob Gounley went on to become a deputy team chief for Galileo's engineering team and understands that it is against regulations to hang banners off the sides of buildings without prior approval. Having recently started work on a new project, he now observes the Galileo project from afar. He looks forward to celebrating Galileo's arrival at Jupiter next week. Steve Collins
November 20, 1995
I am a subsystem engineer for the Attitude and Articulation Control
System (AACS). One of the things that makes my job so cool is that I get
to work on LOTS of different things. Here is the stuff I worked on this
week:
I have a computer program that I wrote that draws "Sphere plots." They
are kind of like drawing pictures on the surface of a computerized globe.
This turns out to be a very good way to look at geometry problems for
spacecraft because you can think of the globe as the sky and plot some
stars and planets on it, and then mark where the spacecraft is pointed
and the camera is looking.
I used a program called SKYBALL a lot this week. On the 7th of December
we are going to use a small antenna (called the Relay Radio Antenna, or
RRA for short) to pick up the science data from our probe as it enters
Jupiter's atmosphere. To make it all work, this antenna has to be pointed
at exactly the spot where the probe is. I was asked to make one last
quadruple check of the commands that the spacecraft will use to point
the antenna, so I used my Sphere Plot program to make a picture of
where the Earth and Sun and Jupiter will be on Dec. 7 and then plotted
where the spacecraft's spin axis was pointed and where the commands
will point the antenna. Everything checked out fine.
I also used SKYBALL to see where one of the science instruments was
pointed to help the scientists understand their data better. I build lots of
little programs to plot or compute things, so knowing how to work with
and program computers is very important for my job. My little programs
are like a set of *tools* and I have a "toolbox" of my favorites that I use
and work to improve all the time.
I went to a meeting to figure out how to use our not-quite-healthy tape
recorder to play back the data we record from the probe. The meeting
was long and there was lots of heated debate over the way to get the job
done. In the end the project manager put off the decision till later and
give the anomaly team (the group of people working on the problem) a
little more time to work. It's pretty common for "decision" meetings to
end this way.
I'm helping the tape recorder anomaly team by finding, plotting and
looking at lots of telemetry from the tape recorder (I'll write about how I
ended up doing this in another message).
I wrote a little program to look through a whole bunch of tape recorder
telemetry (the signal that we receive from the spacecraft) and pull out
just the data when the recorder was playing or recording at its lowest
speed. Some folks are working on some new software for the spacecraft
that will automatically check to see if the tape recorder is slipping or
acting funny. If it is, the new software will respond by stopping the
recorder. The people working need to know how much power the tape
recorder uses at different places on the tape and how much it changes
I also found some data on the pressure inside the recorder's sealed case.
It turns out that the pressure also serves as a sensitive measure of the
*temperature* of the recorder. This is a good example of how we
sometimes have to use things (and data) in ways that were not originally
intended.
Well, that's all the stuff I can think of at the moment. I'll write again
soon...
Steve
Randy G. Herrera November 20, 1995 Well, the Radio Science crisis I described in my last journal has subsided. We discovered early last week that there were software changes in the July upgrade which only the programmers knew about. We (the users) didn't. AAARGHHH! So, now at least we know what the problem is (one computer is too slow compared to another computer and so it is dropping information in the process). Luckily, we do have some ways to work around this. It's almost 7 pm on Tuesday night before Thanksgiving and The Smiths are serenading me as I type this. I just finished editing our Radio Science Handbook. This is a resource document that our team puts together right before every major experiment. We list useful things like phone numbers and beeper numbers. We also explain the different parts of our instrument (both the Deep Space Network (DSN) part and the spacecraft part). We list the individual responsibilities of the members of the Support Team. There's a section on references that we use and monitoring systems that are useful to us. There's a section on procedures that are common to all of our experiments. And, finally, we explain each of the upcoming experiments including the appropriate setup for the Radio Science System at the DSN ground stations. Well, I'm finally done and tomorrow I will take it into the documentation section to be photocopied. Whew!! (See--language skills are very IMPORTANT!) Have I spoken about our BIG experiment on December 8? Well, I'll just tell you about it anyway (hee hee). On December 8, the day after we reach Jupiter orbit, the spacecraft will go "behind" Jupiter as seen from Earth. This is called an "Earth Occultation by Jupiter." As the spacecraft begins to move behind the planet, the radio signal will begin to pass through the Jovian atmosphere. The atmosphere acts like a lens and it will bend (or "refract") the radio signal. We will record the signal at the ground station (for this experiment, it will be the one in Madrid) using special equipment. For radio science, we really are only interested in the center of the signal called the carrier. The equipment at the ground station will sample the carrier at the rate of 5000 times per second and we will record the signal for almost three hours. Now, the navigation team knows the position of the spacecraft really well. So, by combining the navigation information with the information from the recorded radio signal, our Radio Science investigators can develop what's known as a refractivity profile (that is, they can show refraction as a function of height above the planet). The neat part is that we can actually use this information to examine what's in Jupiter's atmosphere! The investigators have a pretty good--but not perfect--idea of the composition of Jupiter's atmosphere. Different mixtures of gases will have different refractive effects on the radio signal. So, they'll fine tune their composition "model," changing around the mixture of gases until the model gives them a refractivity profile like what they see in the data. Then, based on gas physics, they can determine temperature and pressure profiles along the path of the radio signal--all from a distance far above Jupiter's atmosphere. Pretty Cool, huh!! The next two weeks will be spent making final preparations for the Experiment. It actually begins at 2:02 AM on Friday, December 8 (yes, that's 2 in the morning!). But, we have lots of things to do before then. In fact, by the time it starts, we shouldn't have anything to do (if all goes well)! We'll just sit back and watch as the station records our data. Well, that's all for now. Ciao, Randy G. Herrera If this is your first message from the updates-jup list, welcome! To catch up on back issues, please visit the following Internet URL: http://quest.arc.nasa.gov/galileo/journals/index.html |
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