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Odyssey Orbit Insertion: Minute-by-Minute


posted: 07:10 am ET
23 October 2001
ET

Untitled Document

Mars Orbit insertion is the point in the mission when the Odyssey spacecraft arrives just short of Mars, fires an onboard rocket to slow its speed relative to the planet, and is captured into a long looping orbit. Here are the details of what is planned for the Odyssey spacecraft in order for it to go into orbit around Mars tonight, according to NASA's Jet Propulsion Laboratory:

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SCHEDULE OF EVENTS

If all goes well, this is what will happen, minute-by-minute.

All times p.m., ET:

7:56 About two-and-a-half hours before the engine firing, commands are sent to fire small onboard thrusters to "desaturate" or unload the momentum of the spinning reaction wheels. These devices are similar to gyroscopes and are used to control the spacecraft's orientation - its positioning in three axes - so that it is facing the desired direction. The desaturation readies the reaction wheels for the task of turning Odyssey into the proper pointing position for the orbit insertion engine firing.

10:06 Catalyst bed heaters, called "catbed" heaters, are turned on to warm the "catbeds" to an operational temperature for more efficient operation of the reaction control thrusters. These small jets control the spacecraft's position in three axes: pitch, yaw and roll. They will fire intermittently during the main engine firing to keep the spacecraft on an even keel.

10:12 The lines from the fuel and oxidizer tanks to the main engine (which were vented of any residual gas before launch) are now filled by opening pyrotechnic valves. Five minutes later, the fuel and oxidizer tanks are pressurized by opening additional pyrotechnic valves to ensure an even and steady flow of fuel and oxidizer during the engine operation. This is important to provide smooth combustion within the engine for stable thrust and steady deceleration of Odyssey.

(Propulsion system valves for filling the lines and pressurizing the tanks are activated when small pyrotechnic charges are electrically ignited to open valves in tubing about the diameter of a pencil. Each charge breaks open a seal and creates a clear line to allow the pressurant - helium gas - to flow into the tanks. gasses to flow freely into the empty tubes.)

10:18 Telecommunications channels are switched from the spacecraft's high-gain antenna to the medium gain antenna for transmission of a carrier signal to the Earth, and to the low-gain antenna for receipt of commands from the Earth. These antennas are less powerful, but they can receive and send signals from through a wider arc than the high-gain antenna. Only the carrier signal -- which includes no telemetry -- will be transmitted from now until the spacecraft has emerged from behind Mars into full view of the Earth. At that time, the spacecraft will have completed its engine firing and been captured by the Martian gravity into a large elliptical orbit around Mars.

10:19 The 70-meter (230-foot) diameter antenna of the Deep Space Network complex in Goldstone, Calif., locks on to Odyssey's carrier signal. Receipt of this signal will allow ground controllers to gauge the spacecraft's motion by the changes in the carrier frequency. These changes, called Doppler shift, will occur as the spacecraft's velocity changes during the main engine firing. Reaction wheels now turn the spacecraft to face the proper direction in preparation for the engine firing.

10:26 Ignition of the main engine starts for the Mars orbit insertion.

10:36 The Deep Space Network loses the spacecraft signal as Odyssey passes behind Mars. "The next 20 minutes will likely be the longest 20 minutes of our lives," says Odyssey Mission Manager David A. Spencer.

10:36 Still behind Mars and incommunicado, the spacecraft enters Mars' shadow and darkness for two minutes.

10:39 Odyssey reaches periapsis - the lowest point in its first orbit of Mars, at an altitude of about 328 kilometers (203 miles). It is still out of reach of Earth ground stations.

10:45 The main engine firing is now complete.

10:49 Still out of touch with the Deep Space Network, Odyssey's reaction wheels turn the spacecraft to point the high-gain antenna toward Earth. Fault protection software that was turned off during the important orbit insertion phase orbit insertion firing is turned on again. (Fault protection software overrides normal spacecraft operations when an unexpected event occurs on the spacecraft, and directs the spacecraft to stop what it's doing, place itself in a safe state and orient itself to await further commands from Earth. Fault protection software is turned off during important single-opportunity events to prevent such an override from interfering with accomplishing these events.)

10:56 From Earth's point of view, Odyssey emerges from behind Mars, and the Deep Space Network antennas seek to lock on to the spacecraft's carrier signal.

11:00 Odyssey's propellant, oxidizer and pressurant tanks are mechanically isolated with pyrotechnically activated valves so the propellant tanks will not be overpressurized.

11:01 Odyssey turns on its telemetry and begins transmitting data at 40 bits per second. The Deep Space Network will take several minutes to synchronize their equipment with the pattern in the telemetry because of the slow rate at which the data is being received. Once the Deep Space Stations' equipment has locked on to the signal, the messages from Odyssey will be forwarded to JPL.

Then what? Assuming all goes as planned, Odyssey will spend about 1 hour downloading data from the maneuver. By around 1:30 to 2 a.m. ET on Oct. 24, the team should have analyzed the data and announced the fate of the mission. SPACE.com will provide full coverage.

What will happen during Mars Orbit Insertion?

Odyssey will approach Mars at a speed of 5.907 kilometers per second, or 13,214 miles per hour. At a distance of 1,547 kilometers (961 miles) from Mars, the spacecraft is readied for the engine firing that will brake its approach speed and allow Odyssey to be captured into Mars' orbit.

The Mars orbit insertion "burn," as it is called, is the sole purpose of Odyssey's main engine. The 266 kilograms of propellant (587pounds) of hydrazine fuel and nitrogen tetroxide oxidizer that will mix in the controlled combustion of the engine firing represent nearly half the weight of the entire spacecraft. The engine provides 695 newtons, or 156 pounds of thrust.

As a result of the burn, Odyssey's speed will change by 1.420 kilometers per second or 3,176 miles per hour. The 19.7-minute burn will reduce the spacecraft's speed, relative to Mars, to 4.582 kilometers per second, or 10,250 miles per hour.

Step One: Turn off the Fault Protection Software

One of the first steps in the orbit insertion process is to turn off "fault protection" software onboard Odyssey. This software is a block of special commands that override normal spacecraft operations when an unexpected event occurs on the spacecraft.

The commands direct the spacecraft to stop what it's doing and point its antenna toward Earth to await further commands in a so-called "safe" mode. Fault protection software is turned off during maneuvers like engine firings to prevent such an override from interfering with critical events.

Step Two: Fire the Onboard Thrusters

About two-and-a-half hours before the engine firing, commands are sent to fire small onboard thrusters to "desaturate" or unload the momentum of the spinning reaction wheels. These devices are similar to gyroscopes and are used to control the spacecraft's orientation - its positioning in three dimensional space (x, y and z axes) - so that it is facing the desired direction.

Step Three: Check the Spacecraft's Heading

Thirty minutes before the firing, the Odyssey team takes a reading from the spacecraft's accelerometer and performs last minute calculations to ensure that the spacecraft is precisely where it is supposed to be. This is the last opportunity to change any parameters, such as timing or direction, of the main engine firing that's about to take place.

Step Four: Turn on the Heat

In the remaining minutes, a number of major electrical, mechanical and communications events take place onboard: catalyst bed heaters, called "catbed" heaters, are turned on to prime the reaction control thrusters in preparation for firing.

These small jets control the spacecraft's position in three axes: pitch, yaw and roll, and will fire intermittently during the main engine firing to keep the spacecraft on an even keel. A second set of electrical heaters is turned on to warm the main engine system in preparation for its firing.

Step Five: Fill Engine Lines with Propellant and Pressurize

The fuel and oxidizer tanks now must be pressurized to ensure an even and complete flow of all the propellant during the engine firing. A series of valves must be opened for pressurization to take place. This is accomplished through two small pyrotechnic charges that are electrically ignited to open valves in tubing about the diameter of a pencil.

If fired in a lab on Earth, the firing of the "pyro valves" as they are called would be as loud as a firecracker. But in the soundless vacuum of space, of course, the pyro firings will be silent. Each charge breaks open a seal and creates a clear line to allow the pressurant -- helium gas -- to flow into the fuel and oxidizer tanks.

In about one minute, the oxidizer and fuel tanks will have reached their proper pressure to begin engine firing, which occurs about seven minutes after pressurization begins.

Step Six: Get Ready for Telecommunications

Telecommunications channels are switched from the spacecraft's medium-gain antenna to the low-gain antenna for receipt of commands. The low gain antenna is less powerful, but its can receive and send signals from more angles than the medium-gain antenna.

Only the carrier signal - the spacecraft's engineering "heartbeat," which includes no data - will be transmitted from now until about an hour. At that time, the spacecraft will have completed its engine firing behind Mars and reemerged to resume telecommunications with Earth.

The 70-meter antenna of the Deep Space Network complex in Goldstone, California locks on to Odyssey's carrier signal. Receipt of this signal will allow ground controllers to gauge the spacecraft's motion and the changes in frequency, called Doppler shift, that occur as the spacecraft's velocity and direction changes during the maneuver. Reaction wheels now turn the spacecraft to face the proper direction in preparation for the engine firing.

Step Seven: Commence Firing

A solenoid-actuated valve is electrically opened to allow fuel and oxidizer to flow into the main engine injector. This showerhead-like assembly directs streams of fuel and oxidizer at each other to ensure they will mix in the rocket combustion chamber. When the two mix, they combust, starting the controlled explosion of the spacecraft's 19.7 minute-long firing.

JPL propulsion specialist Carl Guernsey describes what the Mars orbit insertion maneuver would look like up close:

"If you were flying alongside of the spacecraft, you would see the engine start to glow around its throat." As they heated with the burning propellant, parts of the engine and rocket nozzle would emit a reddish-to-white glow. The rocket exhaust, he said, might show up as a translucent, faint blue or white glow, but most of the engine firing would be invisible to human eyes.

Flexible extensions on the spacecraft, such as the solar panels, will vibrate lightly in response to the initial engine firing. The small reaction control thrusters strategically mounted on various parts of the spacecraft will fire to correct any oscillation in the spacecraft's orientation. This keeps the main engine pointed in the right direction.

Step Eight: Hold Your Breath

The firing continues as the spacecraft passes behind Mars, and the Deep Space Network will temporarily lose the spacecraft signal. This may be the most excruciating time for flight controllers. As though awaiting word on their baby from the delivery room, the expectant parents of Mars Odyssey must withstand the silence and trust that all's going as planned. Still incommunicado behind Mars, the spacecraft enters Mars' shadow and flies in darkness for two minutes.

Odyssey reaches periapsis - the lowest point in its first orbit of Mars -- at an altitude of about 328 kilometers (203 miles). When the firing is complete, Odyssey is still behind Mars and out of reach of Earth ground stations.

Step Nine: Communicate with Earth

The Odyssey team now stands by and waits for their spacecraft to break the long silence and report on its condition. On the spacecraft itself, Odyssey's reaction wheels turn the spacecraft to point the high-gain antenna toward Earth to prepare for resumption of communications with Earth. Fault protection software that was turned off during the orbit insertion firing is turned on again.

At last, from Earth's point of view, Odyssey emerges from behind Mars, and the Deep Space Network antennas seek to lock on to the spacecraft's carrier signal. Onboard Odyssey, latching valves close to isolate propellant, oxidizer and pressurant tanks from one another so that no mixing of residual chemicals can occur.

The spacecraft begins transmitting data at 40 bits per second; the Deep Space Network will take several minutes to lock on to the low-rate data stream.

Navigators expect that Odyssey will be captured into an initial orbit that will take between 15 and 25 hours for the spacecraft to round the planet. If the orbit is greater than 22 hours, flight controllers will command the spacecraft to fire its small thrusters to lower the spacecraft's altitude so that it takes no more than 20 hours to circle the planet.

Return to Odyssey Special Report


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