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At least 1,711 records · Page 95

(abstract) Telecommunications for Mars Rovers and Robotic Missions

Telecommunications plays a key role in all rover and robotic missions to Mars both as a conduit for command information to the mission and for scientific data from the mission. Telecommunications to the Earth may be accomplished using direct-to-Earth links via the Deep Space Network (DSN) or by relay links supported by other missions at Mars. This paper reviews current plans for missions to Mars through the 2005 launch opportunity and their capabilities in support of rover and robotic telecommunications.

robots rovers telecommunications Mars Mars Pathfin↗

Rover Technology for Mars Surface Exploration

Provided is an overview of emerging technologies in miniaturized roving vehicles that enable new types of low-cost planetary missions, those which are aimed at detailed survey of extended surface areas, collection and analysis of interesting samples, and in-situ analysis of scientific data. New types of planetary surface data can be acquired at low-cost through the use of innovative technologies.

Mars Rover Surface Exploration Pathfinder↗

Development of In Situ Instruments for Planetary Exploration - Unique Challenges in Design, Development, and Execution

A viewgraph presentation describing in situ instruments for NASA missions is shown. The topics include: 1) In Situ Instrumentation; 2) Planetary Extremes; 3) Mars Surface Environment; 4) Lunar Precursor Mission Environment; 5) Europa Surface Analogue; 6) Other Parameters; 7) Space In Situ Instrumentation still in its Infancy; 8) Needed Capabilities For In Situ Science; 9) Framework For Putting The Pieces Together; 10) The Wild World of Astrobiology; 11) Timeline; 12) Example: MOD; 13) In Situ Sample Analysis Laboratories are more complex; 14) technologies In Situ Sample Analysis Requires Integration of Many Emerging Advanced Concepts; 15) Supporting technologies for In Situ Laboratories; 16) Micro-laboratory example; 17) In Situ Instrument Classes; and 18) Key for Analytical Instrument:Sample Preparation.

In Situ Instrumentation↗

The Challenges of Landing on Mars

Humans have been fascinated with the idea of exploring Mars since the very beginning of the space age. Largely due to the belief that life may have at one time existed in some form, surface exploration has been the ultimate ambition of this exploration. Unfortunately engineers and scientists discovered early on that landing a spacecraft on the surface of Mars was to become one of the most difficult and treacherous challenges of robotic space exploration. At arrival to Mars, a spacecraft will be traveling at velocities between 4 and 7 km/s. 100% of this kinetic energy (KE) must be safely removed for a lander to deliver its payload to the surface. Fortunately Mars has an atmosphere substantial enough to allow the combination of a high drag heatshield and a parachute to remove 99% and 0.98% respectively of this kinetic energy. Unfortunately the atmosphere is not substantial enough to bring a lander to a safe touchdown. This means that an additional landing system is required to remove the remaining kinetic energy. On all previous successful missions the landing system has consisted of 2 major elements, a propulsion subsystem to remove an additional 0.002% (approx.50 - 100 m/s ) of the original KE and a final dedicated touchdown system. The first generation Mars landers used legs to accomplish touchdown. The second generation of Mars lander touchdown systems used airbags to mitigate the last few meters per second of residual velocity. NASA is currently developing a third generation landing system in an effort to reduce cost, mass and risk while simultaneously increasing performance as measured by payload fraction to the surface and accessible terrain roughness.

sky cranes↗