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(From Aviation Week's Aerospace Daily & Defense Report, June 5, 2007)
NASA to Instrument Mars Science Laboratory Heat Shield for Aerodynamics Data
NASA's exploration, science and aeronautics directorates have joined
forces to instrument the heat shield for the upcoming Mars Science
Laboratory (MSL) mission to gather aerodynamics data that could help
eventually land human astronauts on the red planet. Set to launch in the
fall of 2009 and arri ve the following summer, the 1- metric ton MSL will
be the largest payload ever landed on Mars.
Ordinarily, NASA's science directorate wouldn't have bothered
instrumenting the heat shield due to the expense involved, according to
Scott Horowitz, head of NASA's Exploration Systems Mission Directorate
(ESMD). But both ESMD and the Aeronautics Research Mission Directorate
(ARMD) saw MSL as an opportunity to gather needed data. "Aeronautics is
very interested in the basic science of aero and how good are their
models at predicting how the heat shield works on Mars," Horowitz said.
And "it's obviously very useful engineering information for us as we
start developing the heat shield for the future, because we're going to
eventually go to Mars."
Every mission NASA has landed on Mars has used versions of the parachute
system originally developed and qualified for the Viking landings of the
1970s, according to Peter Coen, principal investigator for the ARMD
supersonics project. MSL "will be the absolute limit of what that
parachute system can safely land," Coen told The DAILY. For anything
larger, "we're going to need a different kind of system."
The estimated landing mass for a human mission to Mars is 20 metric
tons. The Apollo Earth re-entry approach of heat shields and parachutes
took advantage of Earth's denser atmosphere, but similar systems
wouldn't provide enough deceleration at Mars. Martian landings have used
an aeroshell for hypersonic (i.e., greater than Mach 5) deceleration,
followed by parachutes for supersonic deceleration. Possible higher-mass
concepts include a larger aeroshell that could handle both hypersonic
and supersonic deceleration.
NASA has up to this point worked these problems separately, "knowing all
along that what we really need to do is solve that problem together"
with a single system, Coen said. So the hypersonics and supersonics
researchers at ARMD have joined forces to look at tool and concept
development. The team is looking at parachute-derived concepts for a
2-metric ton landing, and inflatable decelerators or aeroshells with the
potential for supersonic propulsive deceleration as potential solutions
at the 20-metric ton level.
At this early stage, ARMD is focusing on refining its analytical tools
rather than developing specific concepts for Mars entry systems, which
will be driven by ESMD requirements that won't be finalized for many
years. When ESMD is ready, ARMD plans to deliver to them a computational
toolkit along with some "preferred concepts," Coen said.
- Jefferson Morris
Copyright 2007 The McGraw-Hill Companies, posted with permission
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Mars Science Laboratory is part of NASA's Mars Exploration Program, a
long-term effort of robotic exploration of the red planet.
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