Posts Tagged ‘JPL missions’

Highs and Lows of Exploring the Giant Asteroid

Friday, March 2nd, 2012

By Marc Rayman

As NASA’s Dawn spacecraft investigates its first target, the giant asteroid Vesta, Marc Rayman, Dawn’s chief engineer, shares a monthly update on the mission’s progress.

Artist's concept of the Dawn spacecraft soaring over the giant asteroid Vesta.
This artist’s concept shows NASA’s Dawn spacecraft orbiting the giant asteroid Vesta. The depiction of Vesta is based on images obtained by Dawn’s framing cameras. Image credit: NASA/JPL-Caltech |
› Full image and caption

Dear Ups and Dawns,

Dawn is continuing its exploits at Vesta, performing detailed studies of the colossal asteroid from its low altitude mapping orbit (LAMO). The robotic ambassador is operating extremely well on behalf of the creatures it represents on a distant planet. On this second intercalary day of its ambitious adventure, the spacecraft is doing exactly what it was designed to do: exploring a previously uncharted alien world.

Although we usually describe LAMO as being at an average altitude of 210 kilometers (130 miles), that does not mean it is at a constant altitude. As we saw on the fourth anniversary of Dawn’s departure from Earth, there are two reasons the spacecraft’s height changes. One is that the elevation of the surface itself changes, so if the probe flew in a perfect circle around Vesta, its altitude would vary according to the topography. Like the planet from which Dawn embarked upon its deep space journey in 2007 (and even some of the residents there), Vesta is broadest near its equator, and that is where the ground generally reaches its greatest distance from the center. In addition, the ancient surface, battered over billions of years in the rough and tumble of the asteroid belt, displays remarkable variations in shape. The giant Rheasilvia basin is a scar from an extraordinary impact that excavated a region encompassing the south pole more than 500 kilometers (over 300 miles) in diameter. This immense gouge has left that part of Vesta at a much lower elevation than elsewhere. In the center of the enormous depression is the second tallest mountain known in the solar system, soaring to well over twice the height of Mt. Everest. The vertical range from the highest locations near the equator to the bottoms of the deepest craters within Rheasilvia is more than 60 kilometers (37 miles). So as Dawn loops around in just over four hours, the surface underneath it rises and falls dramatically.

The second reason is that the orbit itself is not exactly a circle. Let’s ignore for a moment the effect of the topography and focus solely on the shape of the craft’s path around Vesta. As Vesta rotates and Dawn revolves, the gravitational forces acting on the orbiter are always changing because of the irregular distribution of material inside the geologically complex protoplanet. This effect occurred at the higher altitudes as well, but it was much less pronounced there. Now that the adventurer is deep in the gravity field, the peaks and valleys of its own motion are magnified.

Navigators were very careful in choosing the parameters for LAMO, recognizing that the orbital waters were turbulent. Nevertheless, their mapping of the gravitational currents proved quite accurate, and the spacecraft has followed the planned course quite well. The lengthy and relatively technical discussions in the two previous logs described why the ship drifts off a little, but operators occasionally nudge it back with the ion propulsion system.

Orbits usually are best described by ellipses, like flattened circles. Now Vesta’s bumpy gravity field does not allow perfectly smooth, regular orbits at low altitude. Moreover, the variations in the strength of the gravitational attraction transform the orbits. Sometimes, the difference between the high point of a loop and the low point is less than 16 kilometers (10 miles). As the changing forces reshape the orbit, the ellipse gets more exaggerated, with the low points going lower and the high points going higher. The differences within one revolution grow to be more than 75 kilometers (47 miles). Thanks to the ingenious design of the orbital trajectory however, those same forces then will gradually attenuate the profile, causing it to become more round again. This pattern repeats every 11.5 days in LAMO. It is almost as if the orbit breathes slowly, its envelope expanding and contracting.

› Continue reading Marc Rayman’s Dawn Journal


Mission Control to Mars: Launching the Next Mars Rover

Monday, November 28th, 2011

By Rob Manning

In the wee morning hours of Nov. 26, 2011, scientists and engineers gathered in the mission control room at NASA’s Jet Propulsion Laboratory to help launch the next Mars rover, Curiosity. The mission’s chief engineer, Rob Manning, shares the developing story from the control room as tensions and excitement for a mission eight years in the making reached all new heights.

NASA's Mars Science Laboratory spacecraft, sealed inside its payload fairing atop the United Launch Alliance Atlas V rocket
NASA’s Mars Science Laboratory spacecraft, sealed inside its payload fairing atop the United Launch Alliance Atlas V rocket, launched on Nov. 26 from Kennedy Space Center in Florida.

5:45 a.m. PST (L-01:17:00)
I drove in this morning at 4:30 a.m. As usual, I was greeted by the cheery guards at the gate along with a small family of local deer, who keep sentry over a small patch of greenery at NASA’s Jet Propulsion Laboratory.

I quickly march into JPL’s mission control area to find the first shift quietly following the prelaunch procedure in sync with the Assembly, Test and Launch Operations (ATLO) procedure. They had been on station since 1:30 a.m. I tried that procedure at last week’s launch rehearsal and found the hour a bit unpleasant. Today, I am working on the Anomaly Response Team (ART) for post-launch anomalies. This means that if all goes well, I will have little to do but cheer when NASA’s Mars Science Laboratory rover launches. I have my own console where I can monitor both the spacecraft and listen to the voice nets (there are 10 of them!).

There are about 30 people here. Usually there are not as many, but today we have two people for every subsystem: power, thermal, propulsion, systems, fault protection, attitude control and management. I can hear the JPL ATLO test conductor, Art Thompson, at NASA’s Kennedy Space Center in Florida double check that the right sequence files have been sent. One in particular has commands that tell the rover when to automatically transition into “eclipse” mode. This software mode puts the entire vehicle into the configuration needed for the period prior to separation from the Centaur. In particular this mode turns on the descent stage and cruise stage tank heaters. This timer should be set about 15 minutes after launch, which is planned for 7:02 am PST today. It is an absolute time so they have to send a new time every time we have a new launch attempt. The voice net that is the most interesting is the launch vehicle’s fueling operations. I have not heard that one before. They are more than 50 percent of the way through fueling!

It is fun to see the crowd here. No dress code, but some have come in ties, others with pink mohawks. Nice combo. Professionals all. The peanuts have already made the rounds.

6:15 a.m. (L-00:47:00)
Brian Portock, today’s flight director at JPL, just finished the launch poll of the room to see if everyone is go for transition to launch mode. This is a command to the rover that will put everything on the rover into a mode that is used for the first 15 minutes of flight. In particular, the heaters are all put into a launch and cruise configuration. We expect that the cruise stage heaters will be on more than off due to the air conditioning needed to keep the spacecraft cool (hot generators, you know).

6:29 a.m. (L-00:33:00)
Arm pyros! Once these relays are closed, they will be that way for the next 8.5 months.

6:32 a.m. (L-00:30:00)
The data rate is lowered to launch nominal to 200 bits per second. This will allow the rover’s data to flow to both the ground (via wires to the power van at the foot of the launch pad that provides power to the rover before launch) and to the launch vehicle where it will be available throughout launch (very cool). The JPL management showed up. Charles Elachi is behind me. My old friend and JPL Chief Engineer Brian Muirhead is here with his family.

6:40 a.m. (L-00:22:00)
The flight director is doing the launch poll for the team here at JPL: “All stations at JPL report go.” ATLO is going through its poll at lightening speed. All stations go. This is going fast! The weather guys report of scattered skies at 5,000 feet looks good. I am getting excited.

6:47 a.m. (L-00:15:00)
We lost the flow of data from MSL via the Atlas Space Flight Operations Center (ASOC) land lines, but they switch it to the radio path from the launch vehicle, and it starts flowing again.

7:00 a.m. (L-00:02:00)
All Quiet. Peanuts going around the room again … everyone is excited!

7:01 a.m. (L-00:01:20)
Everything is armed …

7:01 a.m. (L-00:00:30)
GO ATLAS! GO CENTAUR!

7:03 a.m. (L+00:01:00)
GO, GO, GO!

7:06 a.m. (L+00:04:00)
Fairing falls off! Wind on MSL ;)

7:07 a.m. (L+00:05:00)
Rob Zimmerman, our power systems engineer, reports power on solar arrays! 3.3 x 2 = 6. 7 amps! The spacecraft is still power-negative for a while which means that the battery is still discharging. We need more sunlight - very soon.

7:11 a.m. (L+00:09:00)
Getting intermittent data from the rover via the Centaur. So far, no computer reboots!

7:12 a.m. (L+00:10:00)
The ATLO test conductor reports that they are done building and launching MSL (hey, it took ‘em long enough! ;) ). We all cheer and smile. They are supporting the cruise team now.

7:14 a.m. (L+00:12:00)
We’ve reached the end of the first burn (MECO1). All is well. Eighteen minutes to second burn. Battery is charging at 4.3 amps for each battery — very good.

7:17 a.m. (L+00:15:00)
The eclipse-mode transition should be done; don’t know yet. Got it. The tank heaters should be on now; They are. Batteries are still charging at 95 percent state of charge (SOC).

7:35 a.m. (L+00:33:00)
Waiting for telemetry from over Africa …

7:36 a.m. (L+00:34:00)
It’s five minutes to MECO2, pushing out of Earth orbit. Heavy rover! KEEP PUSHING! Mars awaits.

7:39 a.m. (L+00:37:00)
The spacecraft is nearly out of Earth orbit, six minutes until separation from Centaur upper stage. Everyone is relaxed, but there’s not a lot of data from the rover. It still says it is in launch mode — missed the data that said eclipse.

7:42 a.m. (L+00:40:00)
MECO2. next is turn to separation attitude and spin up. Separation! We get a beautiful view of MSL spinning away from us — in the right attitude and the right direction! (› See Video)

The
Video: The Mars Science Laboratory spacecraft separates from the upper stage of its Atlas V launch vehicle and heads on its way to Mars.
› See video

7:53 a.m. (L+00:51:00)
We have lock from NASA’s Deed Space Network in Canberra, Australia!

8:07 a.m. (L+01:05:00)
Data-slowing coming … All looks good, batteries at 98 percent. The rover is now in cruise mode. The heaters are on and cycling as designed. The spacecraft is spinning at 2.5 rotations per minute with only 1 degree of nutation (or swaying) — that is not a lot. The Atlas and Centaur did a fantastic job! The generator is working.

8:26 a.m. (L+01:24:00)
Now let’s try the uplink (sweep). Sweep is working! We have strong signals both ways. We are getting two-way Doppler - navigation says that the frequency is just a few hertz off so we had a very nominal injection to solar orbit. We can command!

Everyone is relaxed and trying to see if there is anything that looks wrong, but so far, nothing. Everything is fine. This is weird. Our bird is on its way - it’s where it belongs. We are happy to be in a completely new mode. No more last-minute fixes (to anything but the software). We have a lot to do, but at least our bird is on its way.