54th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronaut 2003
DOI: 10.2514/6.iac-03-j.6.01
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A Status Report on the Characterization of the Microgravity Environment of the International Space Station

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Cited by 9 publications
(11 citation statements)
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“…Inside the vehicle, the quality of weightlessness is influenced by so-called ''g-jitters,'' that is, vibrations caused by onboard machinery, movement of astronauts, thruster operation, and so on. The ''microgravity'' level may range between * 10 -3 to 10 -6 g, depending on the location within the spacecraft and the frequency of vibration (Tryggvason et al, 2001;Penley et al, 2002;Jules et al, 2004). In life-science experiments, we are interested in the impact of mechanical stresses generated through the force of gravity on the mass of the organism.…”
Section: Simulated Microgravitymentioning
confidence: 99%
“…Inside the vehicle, the quality of weightlessness is influenced by so-called ''g-jitters,'' that is, vibrations caused by onboard machinery, movement of astronauts, thruster operation, and so on. The ''microgravity'' level may range between * 10 -3 to 10 -6 g, depending on the location within the spacecraft and the frequency of vibration (Tryggvason et al, 2001;Penley et al, 2002;Jules et al, 2004). In life-science experiments, we are interested in the impact of mechanical stresses generated through the force of gravity on the mass of the organism.…”
Section: Simulated Microgravitymentioning
confidence: 99%
“…The transient component is composed of those accelerations that last for a short period of time, and are non-periodic. The frequency content varies over the entire frequency spectrum of the data [3]. Unlike the quasi-steady component, the vibratory and transient components need to be measured near the location of interest; no reliable mathematical predictions can be made relative the propagation of a vibratory/transient disturbance through the vehicle.…”
Section: Microgravity Environmentmentioning
confidence: 99%
“…Each sensor head has a defined coordinate system whose location and orientation is defined with respect to the Space Station Analysis Coordinate System [4]. Each origin is defined at the triaxial center point of the three accelerometers that comprise the head.…”
Section: Data Measurement Onboard the Iss Configuration -Prior To Colmentioning
confidence: 99%
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