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 The Mars Surveyor 2001 Lander is scheduled for launch on April 3, 2001. It will land on Mars on Jan. 27, 2002, if launched on schedule. The 2001 Lander will carry an imager to take pictures of the surrounding terrain during its' rocket-assisted descent to the surface. The descent imaging camera will provide images of the landing site for geologic analyses, and will aid planning for initial operations and traverses by the rover. After landing, the long-range rover, carrying the Athena instrument payload, will be deployed for a 365-Earth-day mission to collect and store up to 91 rock and 13 soil samples using a mini-coring device. The 2001 Lander will also be a platform for instruments and technology experiments designed to provide key insights to decisions regarding successful and cost-effective human missions to Mars. Hardware on the Lander will be used for an in-situ demonstration test of rocket propellant production using gases in the Martian atmosphere.

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Other equipment will characterize the Martian soil properties and surface radiation environment. The Mars 2001 Lander will give us valuable data about the radiation environment on the surface of Mars. Analyses of Martian dust and soil are necessary to understand any interactions with the systems currently planned that will supply the habitation and working environment for future human explorers.

Lander information - please click on the experiments below for more details.

 

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 Mars Surveyor 2001 Lander - side view and top view3Dlander_side.jpg
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General Description

Detailed Document
Adobe PDF file


2001 Landing Sites Selection Process:

 2001 Landing Sites Workshop NASA Ames Research Center

Mars Landing Site Catalog NASA Ames Research Center


2001 Lander Experiments:

Mars Environmental Compatability Assessment (MECA) information:

Dust and Soil Experiment Chosen For Mars 2001 Mission

 

Mars Descent Imager for Mars Surveyor 98 (similiar to Mars Surveyor 2001 Descent Imager)

Mars Descent Imager (MARDI) for Mars Surveyor 98

 

Mars In Situ Propellant Production (MIP) related information:

Mars Exploration Technology Program:

Mars Ascent Propulsion

Project Slides

 Lander cruise configuration

Lander flight configuration

Lander flight configuration-exploded view

Lander top view

Lander-side view

Lander configuration

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 Lander science payload

Lander science payload - 2

Mars Descent Imager (MARDI)

Martian Radiation Environment Experiment (MARIE)

Mars Environmental Compatability Assessment (MECA)

Mars In Situ Propellant Production (MIP)

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Return to Mars Surveyor 2001 Home Page


 

Refer to our list of contacts to properly direct general inquiries.

For technical questions or comments on this website contact:
Kirk Goodall
(kirk.goodall@jpl.nasa.gov), Mars Web Engineer