Mars Surveyor '98 program

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Mars Polar Lander mission logo M98patch.png
Mars Polar Lander mission logo

The Mars Surveyor '98 program comprised two spacecraft launched separately,[ citation needed ] the Mars Climate Orbiter (formerly the Mars Surveyor '98 Orbiter) and the Mars Polar Lander (formerly the Mars Surveyor '98 Lander); on board the Mars Polar Lander spacecraft were two surface-penetrator probes (Deep Space 2). The two missions were to study the Martian weather, climate, water and carbon dioxide (CO2) budget, to understand the reservoirs, behavior, and atmospheric role of volatiles and to search for evidence of long-term and episodic climate changes.[ citation needed ]

Mars Climate Orbiter robotic space probe launched by NASA on December 11, 1998

The Mars Climate Orbiter was a 338-kilogram (745 lb) robotic space probe launched by NASA on December 11, 1998 to study the Martian climate, Martian atmosphere, and surface changes and to act as the communications relay in the Mars Surveyor '98 program for Mars Polar Lander. However, on September 23, 1999, communication with the spacecraft was lost as the spacecraft went into orbital insertion, due to ground-based computer software which produced output in non-SI units of pound-force seconds (lbf·s) instead of the SI units of newton-seconds (N·s) specified in the contract between NASA and Lockheed. The spacecraft encountered Mars on a trajectory that brought it too close to the planet, and it was either destroyed in the atmosphere or re-entered heliocentric space after leaving Mars' atmosphere.

Mars Polar Lander robotic spacecraft lander launched by NASA on January 3, 1999

The Mars Polar Lander, also known as the Mars Surveyor '98 Lander, was a 290-kilogram robotic spacecraft lander launched by NASA on January 3, 1999 to study the soil and climate of Planum Australe, a region near the south pole on Mars. It formed part of the Mars Surveyor '98 mission. On December 3, 1999, however, after the descent phase was expected to be complete, the lander failed to reestablish communication with Earth. A post-mortem analysis determined the most likely cause of the mishap was premature termination of the engine firing prior to the lander touching the surface, causing it to strike the planet at a high velocity.

Contents

Both spacecraft were launched during the 1998 Mars orbit insertion launch window. Both were lost, including the penetrator probes.[ citation needed ]

Orbit insertion is the spaceflight operation of adjusting a spacecraft’s momentum, in particular to allow for entry into a stable orbit around a planet, moon, or other celestial body. This maneuver involves either deceleration from a speed in excess of the respective body’s escape velocity, or acceleration to it from a lower speed.

Launch window time period during which a space vehicle must be launched in order to reach its intended target

In the context of spaceflight, launch period is the collection of days and launch window is the time period on a given day during which a particular vehicle must be launched in order to reach its intended target. If the rocket is not launched within a given window, it has to wait for the window on the next day of the period. Launch periods and launch windows are very dependent on both the rocket's capability and the orbit to which it is going.

Loss of the orbiter

The orbiter was lost due to a miscalculation in trajectory caused by an unintended and undetected mismatch between metric and English units of measurement. [1] The use of metric units as well as the data formats to employ were specified in a navigation software interface specification (SIS) published by JPL in 1996. Despite this, the flight operations team at Lockheed Martin provided impulse data in English units of pound-force seconds rather than newton seconds. These values were incorrect by a factor of 4.45 (1 lbf = 4.45 N). This caused erroneous course corrections that caused the orbiter to descend too low in Mars's atmosphere. The vehicle either burned up or bounced off into space.[ citation needed ]

English units are the units of measurement that were used in England up to 1826, which evolved as a combination of the Anglo-Saxon and Roman systems of units. Various standards have applied to English units at different times, in different places, and for different applications.

Lockheed Martin Corporation is an American global aerospace, defense, security and advanced technologies company with worldwide interests. It was formed by the merger of Lockheed Corporation with Martin Marietta in March 1995. It is headquartered in North Bethesda, Maryland, in the Washington, DC, area. Lockheed Martin employs approximately 100,000 people worldwide as of December 2017.

Loss of the lander

Investigators concluded that the most likely cause of the lander's failure was a spurious sensor signal associated with the craft's legs falsely indicating the craft had touched down when in fact it was some 40 meters above the surface.[ citation needed ] When the landing legs unfolded they made a bouncing motion that accidentally set off the landing sensors, causing the descent engines to shut down prematurely and the lander to fall. Another possible reason for failure was inadequate preheating of catalysis beds for the pulsing rocket thrusters.[ citation needed ] Hydrazine fuel decomposes on the beds to make hot gases that are forced out of the rocket nozzles, generating thrust; in crash review tests cold catalysis beds caused misfiring and instability.

Catalysis chemical process

Catalysis is the process of increasing the rate of a chemical reaction by adding a substance known as a catalyst, which is not consumed in the catalyzed reaction and can continue to act repeatedly. Because of this, only very small amounts of catalyst are required to alter the reaction rate in principle.

Hydrazine is an inorganic compound with the chemical formula N
2
H
4
, called diamidogen, archaically. It is a simple pnictogen hydride, and is a colorless and flammable liquid with an ammonia-like odour.

Thrust reaction force which expels or accelerates mass in one direction

Thrust is a reaction force described quantitatively by Newton's third law. When a system expels or accelerates mass in one direction, the accelerated mass will cause a force of equal magnitude but opposite direction on that system. The force applied on a surface in a direction perpendicular or normal to the surface is also called thrust. Force, and thus thrust, is measured using the International System of Units (SI) in newtons, and represents the amount needed to accelerate 1 kilogram of mass at the rate of 1 meter per second per second. In mechanical engineering, force orthogonal to the main load is referred to as thrust.

The Polar Lander under construction in the NASA lab Mars Polar Lander undergoes testing.jpg
The Polar Lander under construction in the NASA lab

Cost

The Mars Surveyor 1998 program spacecraft development cost US$193.1 million. Launch costs for the Mars Surveyor '98 Program was estimated at US$91.7 million and mission operations at US$42.8 million. [2] The Mars Climate Orbiter was part of NASA's 10-year Mars Surveyor Program,[ citation needed ] with launches every 26 months when the Earth and Mars are favorably positioned.

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Spacecraft manned vehicle or unmanned machine designed to fly in outer space

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Space probe unmanned robotic spacecraft that does not orbit the Earth, but, instead, explores further into outer space

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References

  1. BBC News Sci/Tech "Confusion leads to Mars failure", September 30, 1999. Retrieved 24 June 2014
  2. "Mars Climate Orbiter". National Aeronautics and Space Administration. Retrieved January 19, 2016.