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Date: Fri, 18 Nov 2005 17:00:17 -0800
From: NASA Jet Propulsion Laboratory <[EMAIL PROTECTED]>
To: "[EMAIL PROTECTED]" <[EMAIL PROTECTED]>
Subject: Mars-Bound Nasa Craft Tweaks Course, Passes Halfway Point

MEDIA RELATIONS OFFICE
JET PROPULSION LABORATORY
CALIFORNIA INSTITUTE OF TECHNOLOGY
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
PASADENA, CALIF. 91109.  TELEPHONE (818) 354-5011
http://www.jpl.nasa.gov

Guy Webster (818) 354-6278
Jet Propulsion Laboratory, Pasadena, Calif.

Dwayne Brown (202) 358-1726
NASA Headquarters, Washington

News Release: 2005-164                                          November 18, 
2005

Mars-Bound Nasa Craft Tweaks Course, Passes Halfway Point

NASA's Mars Reconnaissance Orbiter successfully fired six engines for about 20 
seconds
today to adjust its flight path in advance of its March 10, 2006, arrival at 
the red planet.

Since its Aug. 12 launch, the multipurpose spacecraft has covered about 60 
percent of the
distance for its trip from Earth to Mars. It will fly about 40-million 
kilometers (25-million
miles) farther before it enters orbit around Mars. It will spend half a year 
gradually
adjusting the shape of its orbit, then begin its science phase.  During that 
phase, it will
return more data about Mars than all previous missions combined. The spacecraft 
has
already set a record transmission rate for an interplanetary mission, 
successfully returning
data at 6 megabits per second, fast enough to fill a CD-ROM every 16 minutes.

"Today's maneuver mainly increases the speed to bring us to the target point at 
just the
right moment," said Tung-hanYou, chief of the Mars Reconnaissance Orbiter 
navigation
team at NASA's Jet Propulsion Laboratory, Pasadena, Calif.  The intended nudge 
in
velocity is 75 centimeters per second (less than 2 miles per hour). The 
spacecraft's speed
relative to the sun is about 27 kilometers per second (61,000 miles per hour).

Four opportunities for course adjustments were planned into the schedule before 
launch.
Today's, the second, used only the trajectory-correction engines.  Each engine 
produces
about 18 newtons (4 pounds) of thrust.  The first course adjustment, on Aug. 
27, doubled
as a test of the six main engines, which produce nearly eight times as much 
thrust.  Those
main engines will have the big job of slowing the spacecraft enough to be 
captured into
orbit when it reaches Mars. The next scheduled trajectory adjustment, on Feb. 
1, 2006, and
another one 10 days before arrival will be used, if necessary, for fine tuning, 
said JPL's
Allen Halsell, the mission's deputy navigation chief.

The Mars Reconnaissance Orbiter mission will examine Mars in unprecedented 
detail from
low orbit. Its instrument payload will study water distribution -- including 
ice, vapor or
liquid -- as well as geologic features and minerals. The orbiter will also 
support future
missions to Mars by examining potential landing sites and by providing a 
high-data-rate
relay for communications back to Earth.

The mission is managed by JPL, a division of the California Institute of 
Technology,
Pasadena, for the NASA Science Mission Directorate. Lockheed Martin Space 
Systems,
Denver, is the prime contractor for the project and built the spacecraft.

For information about the Mars Reconnaissance Orbiter on the Web, visit
http://www.nasa.gov/mro . For information about NASA and agency programs on the
Web, visit http://www.nasa.gov/home/index.html .

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