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dc.contributor.advisorJeffrey A. Hoffman.en_US
dc.contributor.authorOpperman, Roedolph A.(Roedolph Adriaan)en_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2019-10-11T21:53:19Z
dc.date.available2019-10-11T21:53:19Z
dc.date.copyright2019en_US
dc.date.issued2019en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/122498
dc.descriptionThesis: Ph. D. in Aerospace Systems Engineering, Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2019en_US
dc.descriptionCataloged from PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (pages 163-179).en_US
dc.description.abstractProlonged exposure of a vertebrate musculoskeletal system to the microgravity environment of space leads to a reduction in bone mineral density, muscle mass, strength and endurance. Such deconditioning may impede critical astronaut activities and presents an increased injury risk during flight and when exposed to increased gravity like that of Earth or Mars. Exercise countermeasures are used extensively on the International Space Station to mitigate musculoskeletal deconditioning during long duration spaceflight missions. Despite vigorous exercise protocols, bone loss and muscle atrophy are often observed even when countermeasures are in effect. As a first step in understanding the mechanisms of injury and how on-orbit exercise countermeasures compare to those on the ground, an accurate load sensing system is needed to collect ground reaction force data in reduced gravity.en_US
dc.description.abstractTo date, no means of continuous, high resolution biomechanical force data collection and analysis has been realized for on-orbit exercise. Such a capability may advance the efficiency of these systems in mitigating the incidence of bone and muscle loss and injury risk by quantifying loading intensity and distribution during exercise in microgravity, thus allowing for cause-effect tracking of ISS exercise regimes and biomechanics. By measuring these forces and moments on the exercise device and correlating them with the post-flight fitness of crewmembers, the efficacy of various exercise devices may be assessed. More importantly, opportunities for improvement, including optimized loading protocols and lightweight exercise device designs will become apparent.en_US
dc.description.abstractThe overall goal of this research effort is to improve the understanding of astronaut joint loading during resistive exercise in a microgravity environment through the use of rigorous quantitative dynamic analysis, simulation and experimentation. This is accomplished with the development and evaluation of a novel, self-contained load sensing system. The sensor assembly augments existing countermeasures and measures loads imparted by the crew during exercise. Data collected with this system is used to parameterize a unique musculoskeletal model which is then used to evaluate associated joint reaction forces generated during exercise. The effects of varying body posture and load application points on joint loading were investigated and recommendations for enhancing on-orbit exercise protocols that mitigate both injury and deconditioning are discussed.en_US
dc.description.abstractBy validating the sensor and modeling joint loading during on-orbit exercise as described herein, a unique contribution is made in expanding NASA's capability to continuously record and quantify crew loading during exercise on ISS. Data obtained through the system is used to characterize joint loading, inform and optimize exercise protocols to mitigate musculoskeletal deconditioning and may aid in the design of improved, lightweight exercise equipment for use during long-duration spaceflight, including future missions to Mars.en_US
dc.description.sponsorship"This research effort was supported by a NASA Phase I Small Business Innovation Research (SBIR) contract awarded to Aurora Flight Sciences Corporation with MIT as subcontractor. The contract period of performance spanned from June 2014 through August 2016. Contract number: 2012-11 NNX14CS55C"--Page 6en_US
dc.description.statementofresponsibilityby Roedolph Adriaan Opperman.en_US
dc.format.extent193 pagesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses are protected by copyright. They may be viewed, downloaded, or printed from this source but further reproduction or distribution in any format is prohibited without written permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleEnhanced dynamic load sensor for the International Space Station : design, development, musculoskeletal modeling and experimental evaluationen_US
dc.typeThesisen_US
dc.description.degreePh. D. in Aerospace Systems Engineeringen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc1121186126en_US
dc.description.collectionPh.D.inAerospaceSystemsEngineering Massachusetts Institute of Technology, Department of Aeronautics and Astronauticsen_US
dspace.imported2019-10-11T21:53:18Zen_US
mit.thesis.degreeDoctoralen_US
mit.thesis.departmentAeroen_US


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