Spacecraft in orbit over Mars.

Artist's concept of Mars Climate Orbiter. Credit: NASA/JPL-Caltech

Nation United States of America (USA)
Objective(s) Mars Orbit
Spacecraft MCO
Spacecraft Mass 1,407 pounds (638 Kilograms)
Mission Design and Management NASA / Jet Propulsion Laboratory
Launch Vehicle Delta 7427-9.5 (no. D264)
Launch Date and Time Dec. 11, 1998 / 18:45:51 UT
Launch Site Cape Canaveral Force Station, Fla. / Launch Complex 17A
Scientific Instruments 1. Pressure Modulated Infrared Radiometer (PMIRR)
2. Mars Color Imaging System (Two Cameras) (MARCI)

Results

Mars Climate Orbiter (MCO) was the second probe in NASA’s MarsSurveyor program, which also included the Mars Global Surveyor(launched in November 1996) and Mars Polar Lander (launched in January 1999).

Mars Climate Orbiter was designed to arrive at roughly the same time as Mars Polar Lander and to conduct simultaneous investigations of Mars’ atmosphere, climate and surface. Arrival inorbit was dated for Sept. 23, 1999. MCO would then reach its operational near-circular Sun-synchronous orbit at about 260 miles(421 kilometers) by Dec. 1, 1999.

The satellite was also designed to serve as a communications relay for Mars Polar Lander. After the lander’s mission (lasting threemonths), MCO would have performed a two-year independent mission to monitor atmospheric dust and water vapor and take daily pictures of the planet’s surface to construct an evolutionary map of climatic changes.

Scientists hoped that such information would aid in reconstructing Mars’ climatic history and provide evidence of buried water reserves. After the end of its main mapping mission Jan. 15, 2001, Mars Climate Orbiter would have acted as a communications relay for future NASA missions to Mars.

After launch, the spacecraft was put into a Hohmann transfer orbit to intersect with Mars. It performed four midcourse corrections: Dec. 21, 1998, and March 4, July 25 and Sept. 15, 1999.

At 09:00:46 UT Sept. 23, 1999, the orbiter began its Mars orbit insertion burn as planned. The spacecraft was scheduled to re-establish contact after passing behind Mars, but, unfortunately, no signals were received from the spacecraft.

An investigation indicated that the failure resulted from a navigational error due to commands from Earth being sent in English units (in this case, pound-seconds) without being converted into the metric standard (Newton-seconds).

The error caused the orbiter to miss its intended orbit (87 to 93 milesor 140 to 50 kilometers) and to fall into the Martian atmosphere at approximately 35 miles (57 kilometers) in altitude and to disintegrate due to atmospheric stresses.

Source

Siddiqi, Asif A. Beyond Earth: A Chronicle of Deep Space Exploration, 1958-2016. NASA History Program Office, 2018.

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