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Aerodynamics / Spacecraft propulsion / Fluid dynamics / Airspeed / Hypersonic speed / Mars Science Laboratory / Flight / Technology readiness level / Rocket / Space technology / Spaceflight / Aerospace engineering


Development of Supersonic Retro-Propulsion for Future Mars Entry, Descent, and Landing Systems Karl T. Edquist* and Artem A. Dyakonov†
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Document Date: 2011-06-01 10:52:44


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File Size: 3,25 MB

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City

Viking / Houston / Pasadena / Sunnyvale / Phoenix / Hampton / Mars Viking / /

Company

Jet Propulsion Laboratory / Astronautics A. Component Technologies / SRP / ELORET Corporation / Analytical Mechanics Associates Inc. / Mars Science Laboratory / Aerospace / /

Country

United States / /

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Facility

NASA Langley Research Center / American Institute of Aeronautics / NASA Johnson Space Center / Ashley M. Korzun‡ Georgia Institute of Technology / /

IndustryTerm

last / entry system technologies / cold gas propulsion system / technology effort / technology maturation schedule / technology maturation / little hardware / potential system applications / technology development / targeted landing site / decelerator technology / start-up / engine startup / separate technology development programs / technology development roadmap / hot-gas propulsion system / technology advancement / test hardware / flight systems / technology development effort / entry systems / technology gates / component technologies / decelerator technology option / /

Organization

Phoenix MSL / Phoenix mission / W. Studak§ and Michael A. Tigges¶ NASA Johnson Space Center / Landing Systems Karl T. Edquist* and Artem A. Dyakonov† NASA Langley Research Center / Kerry A. Trumble** NASA Ames Research Center / Senior Engineer / Aeroscience & Flight Mechanics Division / American Institute of Aeronautics / US Federal Reserve / National Aeronautics and Space Administration / Georgia Institute of Technology / Atlanta / Key Performance Parameter Mars Exploration Rover Mars Science Laboratory / Daniel Guggenheim School of Aerospace Engineering / /

Person

Karl T. Edquist / Atmospheric Flight / Aeroscience / Ravi Prakash / Michael A. Tigges / Aerothermodynamics Branch / /

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Position

Research Scientist / model development The identification / Graduate Research Assistant / †† Aerospace Engineer / Systems Analysis Branch / Systems Engineer / Engineer / Major / representative / /

Product

RL / TRLs / /

ProvinceOrState

Texas / Virginia / California / Georgia / /

Technology

2 Technology / thermal protection system Technology / Fluid Dynamics / key technologies / aerothermodynamics databases Developing algorithms / decelerator technology / alternative EDL technologies / EDL technologies / component technologies / Viking-era entry system technologies / simulation / EDL technology / /

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