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Technology
Summary
Technologies of Broad Benefit
In-Situ and Sample Return
bullet Entry, Descent, and Landing
Guided Entry
Powered Descent
Descent Imaging
Bigger Parachute
Sky Crane
bullet Autonomous Planetary Mobility
bullet Technologies for Severe Environments
bullet Sample Return Technologies
bullet Planetary Protection Technologies
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In-situ Exploration and Sample Return Technologies:
Entry, Descent, and Landing: Bigger Parachute
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Mars Science Laboratory's parachute, used to slow the spacecraft down during entry, descent, and landing, is part of a long-term Mars parachute technology develoopment effort. It inherits much from its martian predecessors, the the Viking, Pathfinder, and Mars Exploration Rover missions.

Parachute designs are driven by "loads" (the forces the parachute experiences as it fully inflates). Loads are calculated by using atmospheric density, velocity, parachute drag area, and mass. For the exponentially heavier Mars Science Laboratory mission, the parachute's basic design remained the same, but is about 10 percent larger in area than the one used for the Mars Exploration Rover mission. By comparison, that mission was 40% larger than Pathfinder's parachute.

The ability to land large payloads safely on the surface of Mars enables increasingly sophisticated robotic missions, and might also help pave the way for emplacing the infrastructure that would be needed to support human missions to Mars someday.

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