Technologies of Broad Benefit: Propulsion technologies provide the energy to get to Mars and conduct long-term studies.
Modifying a rocket to "pack a major punch"strap-on solid rocket motors developed for the Delta III launch vehicle. The launch of the MER-B spacecraft was the second use of a core Delta II "Heavy" launch vehicle and the first use of a Delta II "Heavy" launch vehicle with an upper stage.
The use of this rocket for the Mars Exploration Rover mission helped pave the way for many future space missions that will need a bit more energy to send them on their way beyond Earth. The MESSENGER mission to Mercury, the seventh mission selected for NASA's Discovery Program, was launched August 3rd, 2004, on a Delta II heavy. [More on the Mars Exploration Rover launch vehicle.]
The traditional Delta II rocket (used to lift Spirit) has been used to propel many NASA missions into space and has a history of more than 40 uccessful launches, but some spacecraft need more energy to propel them on their way to Mars and other planets.
Reasons for the differencesEvery 26 months, Earth, Mars and the Sun align for the most efficient, least energy-consuming path between Earth and Mars. (For advanced details, see at the JPL website Basics of Space Flight: Launch.)
The launch period for Spirit used close to the minimum energy to get to Mars in the 2003 opportunity, while Opportunity needed more energy to get to Mars. The two vehicles could not be launched at the same time due to restrictions at the launch site and the availability of supporting teams.
Improving precision navigationMissions sent to Mars often have to conduct "trajectory correction maneuvers" to keep the spacecraft on course throughout its 460 million kilometer (286 million mile) voyage to Mars. With these propellant burns, navigators can change the spacecraft's velocity, move it sideways or turn it. Navigators for Spirit put the spacecraft so close to a bull's-eye with earlier maneuvers that mission managers chose to skip the final two optional trajectory correction maneuvers for adjusting course before arrival at Mars. Likewise for Opportunity, only three trajectory correction maneuvers were required to achieve its "interplanetary hole in one," into a crater that revealed the first bedrock seen up-close on Mars.
Technologies associated with these propulsion maneuvers often involve better ways of measuring where the spacecraft is in space so that engineers can determine the appropriate burns needed to tweak the spacecraft's trajectory.
The two traditional tracking methods, ranging and Doppler, were complemented by a newer method called "delta differential one-way range measurement." It adds information about the location of the spacecraft in directions perpendicular to the line of sight. Pairs of antennas at Deep Space Network sites on two different continents simultaneously received signals from the spacecraft, then used the same antennas to observe natural radio waves from a known celestial reference point, such as a quasar. Successful use of this triangulation method can shave several kilometers or miles off the amount of uncertainty in delivering the rovers to their targeted landing sites. Opportunity landed about 24 kilometers (about 15 miles) down range from the center of the target landing area. Spirit made it to within 10 kilometers (about 6 miles) of its intended landing area.