Research opportunities have been identified
for Masters and PhD students as part of the joint program between the
NASA-Langley Research Center (LaRC), the
National Institute of Aerospace (NIA) and
the North Carolina State University (NCSU) departments of
Mechanical and Aerospace Engineering
and Marine, Earth, & Atmospheric Sciences.
Students selected for these opportunities will generally perform their research within
a LaRC research Branch under the direction of Dr. Tolson and a NASA mentor.
Since students will be on-site at NASA LaRC, the program will
be restricted to U.S. citizens and permanent residents.
Students interested in these opportunities should, in a timely manner, contact
Prof. Tolson via e-mail and
visit NCSU
for application instructions.
Potential research opportunities include:
Flight mechanics studies for upcoming and past Mars missions including
MER,
Phoenix and
Mars Science Laboratory, with emphasis on the phase from entry to landing.
Participation in proposals for future planetary missions
Interdisciplinary studies of planetary atmospheric and flight sciences.
Participation in one of the numerous LaRC studies associated with the Moon, Mars, and beyond exploration
initiative including using LIDAR for precision lunar and planetary landing.
Participate in a scale model ballistic flights for crew exploration
vehicle (CEV) abort and tumbling characterization.
Determine spatial and temporal spectra of atmospheric waves at aerocapture and EDL altitudes and evaluation
the effects of atmospheric varability on entry performance.
Participate in post flight analysis of data collected during aerobraking operations of the
Mars Global Surveyor,
Mars Odyssey, or
Mars Reconnaissance Orbiter missions and developing methods to
evaluate spacecraft performance and determine Mars atmospheric properties.
Prof. Tolson also collaborates with other NCSU faculty performing research in other areas
at NASA Langley. Some potential current areas of research in aerospace structures
and structural dynamics include:
Structural concepts for the design of lightweight wings for commercial aircraft.
Concepts for morphing wing cross-sections during flight to optimize performance.
Structural design concepts for a blended wing body commercial aircraft.
Application of stitched composites for aircraft control surfaces.
Thermal, material, and structural concepts for hypersonic cruise vehicles and scramjet engines.
Parameter studies of structural joints for the ARES V rocket.
Modal analysis of the ARES I rocket.
Impact analysis of earth landing procedures for manned capsule reentry
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