WASHINGTON (CNN) -- Failure to convert English measures to metric
values was the root cause of the loss of the Mars Climate Orbiter, a
spacecraft that smashed into the planet instead of reaching a safe
orbit, a NASA investigation concluded Wednesday.
In a scathing report released Wednesday, an investigation board
concluded that NASA engineers failed to convert English measures of
rocket thrusts to newton, a metric system measuring rocket force.
One English pound of force equals 4.45 newtons. A small
difference between the two values caused the spacecraft to approach
Mars at too low an altitude and the craft is thought to have smashed
into the planet's atmosphere and was destroyed.
The report cited other contributing causes to the September 23
failure, including:
Inadequate communications between project teams.
The report also said the mission navigation team was overworked
and not closely supervised by independent experts.
The panel made 10 different recommendations to ensure that a
similar mishap is avoided with the Mars Polar Lander, currently en
route for a December 10 touchdown on the red planet.
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Artist's
conception of the Polar Lander on Mars |
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Initially, NASA officials associated the failure with the
agency's so-called "better-faster-cheaper" approach to unmanned
space exploration -- a philosophy adopted in recent years that
accepts a higher margin of risk in order to launch frequent missions
at lower cost.
But NASA has since conceded that the failure was primarily the
result of human error and that cost-cutting had little if anything
to do with the fiasco.
The spacecraft was to be a key part of the exploration of the
planet. From its position overhead, the Mars Climate Orbiter was to
relay signals from the Mars Polar Lander once it reached the surface
of the planet.
Signs of trouble came early
Months before the Climate Orbiter reached Mars, controllers at
NASA's Jet Propulsion Laboratory saw signs of trouble but failed to
understand the implications until it was too late.
"When the earlier trajectory work was being done it was noticed
that the predictions ... were not as exquisitely accurate as they
normally are," said mission controller Ben Clark of Lockheed Martin
Aeronautics.
Such computer predictions are crucial because Earth-bound
antennas offer controllers a one-dimensional and thus incomplete
picture of where to find a spacecraft. But the discrepancies were so
slight, the team simply discounted the predictions.
The Mars Climate Orbiter was equipped with one large solar array
on one side, which was bombarded with millions of tiny solar
particles as the spacecraft traveled to Mars. This solar "wind"
tended to roll the spacecraft over.
A flywheel on board spun in the opposite direction to correct for
the wind. Each day when it reset by spinning back the other way,
tiny thrusters fired to counteract those forces.
Over a nine-month period, these small thruster activities gave
the spacecraft more of a push off-course than controllers were able
to track with their available data, said Richard Zurek, a project
scientist for the mission.
Will Polar Lander be safe?
The prime contractor for the mission, Lockheed Martin, measured
the thruster firings in pounds even though NASA had requested metric
measurements. That sent the Climate Orbiter in too low, where the
$125-million spacecraft burned up or broke apart in Mars'
atmosphere.
That incident has prompted some 11th hour considerations about
how to safely fly the Polar Lander.
"Everybody really wants to make sure that all the issues have
been looked at," says Karen McBride, a member of the UCLA Mars Polar
Lander science team.
The Polar Lander blasted off on January 3 from Cape Canaveral,
Florida.
The spacecraft is designed to use a robotic arm to dig for water
ice in the martian soil and conduct other science experiments in
Mars' southern polar region
Correspondent Miles
O'Brien and The Associated Press contributed to this
report.
Report Summary:
From the Mars Climate Orbiter Investigation Panel
report
Root cause: Failure to use metric units in the
coding of a ground software file, "Small Forces," used
in trajectory models |
|
Contributing causes:
- Undetected mismodeling of spacecraft velocity
changes
- Navigation Team unfamiliar with spacecraft
- Trajectory correction maneuver number 5 not
performed
- System engineering process did not adequately
address transition from development to operations
- Inadequate communications between project elements
- Inadequate operations Navigation Team staffing
- Inadequate training
- Verification and validation process did not
adequately address ground software
|
Recommendations:
- Verify the consistent use of units throughout the
MPL spacecraft design and operations
- Conduct software audit for specification
compliance on all data transferred between JPL and
Lockheed Martin Astronautics
- Verify Small Forces models used for MPL
- Compare prime MPL navigation projections with
projections by alternate navigation methods
- Train Navigation Team in spacecraft design and
operations Prepare for possibility of executing
trajectory correction
- maneuver number 5
- Establish MPL systems organization to concentrate
on trajectory
- correction maneuver number 5 and entry, descent
and landing
- operations
- Take steps to improve communications
| |
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RELATED SITES:
Mars Polar Lander
Mars Climate
Orbiter/Mars Polar Lander Official Website
Mars Global
Surveyor
Mars Meteorite Home Page
(JPL)
Macquarie
University
Stromatolites
Fossil
Record of the Cyanobacteria
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