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NASA Scientific and Technical Aerospace Reports

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20040111412 <strong>NASA</strong> Marshall Space Flight Center, Huntsville, AL, USA<br />

Automated Detection of Solar Loops by the Oriented Connectivity Method<br />

Lee, Jong Kwan; Newman, Timothy S.; Gary, G. Allen; [2004]; 4 pp.; In English; 17th International Conference on Pattern<br />

Recognition, 23-26 Aug. 2004, Cambridge, UK; Copyright; Avail: CASI; A01, Hardcopy<br />

An automated technique to segment solar coronal loops from intensity images of the Sun s corona is introduced. It exploits<br />

physical characteristics of the solar magnetic field to enable robust extraction from noisy images. The technique is a<br />

constructive curve detection approach, constrained by collections of estimates of the magnetic fields orientation. Its<br />

effectiveness is evaluated through experiments on synthetic <strong>and</strong> real coronal images.<br />

Author<br />

Automatic Control; Coronal Loops; Detection; Solar Corona; Sun<br />

93<br />

SPACE RADIATION<br />

Includes cosmic radiation; <strong>and</strong> inner <strong>and</strong> outer Earth radiation belts. For biological effects of radiation on plants <strong>and</strong> animals see 51 Life<br />

Sciences; on human beings see 52 <strong>Aerospace</strong> Medicine. For theory see 73 Nuclear Physics.<br />

20040111067 Lavochkin Association, Moscow, Russia<br />

On-Orbit Experiments <strong>and</strong> Research on Measuring the Spacecraft Charging<br />

Evgeny, Nikolski; Arcady, Sokolov; 8th Spacecraft Charging Technology Conference; March 2004; 99 pp.; In English; See<br />

also 20040111031; No Copyright; Avail: CASI; A05, Hardcopy<br />

Lavochkin Association is one of the leading enterprises in Russia for about forty years, having specialized in the field of<br />

design <strong>and</strong> manufacturing of tools for orbital injection of payloads <strong>and</strong> automatic vehicles to further study the solar-earth<br />

relationships, the Moon, small heavenly bodies <strong>and</strong> planets of the solar system. A long-term experience of the Association in<br />

the field of space engineering also includes the development of anti-charging protection tools for s/c. This protection is<br />

achieved by means of bonding <strong>and</strong> screening. Originally, two flight experiments on measuring the surface of the s/c charging<br />

have been initiated in 2002 <strong>and</strong> thereafter continued. The purpose of these experiments is as follows: Receiving the data on<br />

relationship between s/c charging <strong>and</strong> operational capability of its systems; Obtaining the experimental data about specific<br />

parameters of the charging; Study of the regularities of the charging process.<br />

Author<br />

Spacecraft Charging; Spaceborne Experiments; Protection; Payloads; Celestial Bodies<br />

20040111069 QinetiQ Ltd., Farnborough, UK<br />

The Flumic Electron Environment Model<br />

Rodgers, D. J.; Hunter, K. A.; Wrenn, G. L.; 8th Spacecraft Charging Technology Conference; March 2004; 13 pp.; In<br />

English; See also 20040111031<br />

Contract(s)/Grant(s): ESA-16265/02/NL/FM; No Copyright; Avail: CASI; A03, Hardcopy<br />

Assessments of the vulnerability of spacecraft materials to internal charging need a good electron environment model.<br />

Since the threat from electrostatic discharges is related to the occurrence of flux enhancements, the st<strong>and</strong>ard mean flux models<br />

are not appropriate. The requirement is for a model of enhanced flux conditions. These tend to occur mainly during the<br />

declining phase of the solar cycle. FLUMIC (Flux Model for Internal Charging) was written to address this requirement. The<br />

model was originally developed as a simple engineering tool. Although simplicity of use is still the philosophy behind<br />

FLUMIC, it has undergone improvements to its accuracy <strong>and</strong> scope, mainly through the inclusion of better data sets <strong>and</strong> more<br />

sophisticated empirical modelling techniques. The latest version, FLUMIC3, has been developed in a new ESA study <strong>and</strong><br />

relies heavily on data from the GOES/SEM <strong>and</strong> STRV-1b/REM instruments. Although the outer belt, including geostationary<br />

orbit, is the region most at risk from internal charging effects, charging currents in the inner belt are not insignificant behind<br />

thin shields. The model now extends to the inner belt so that the current contributions from both inner <strong>and</strong> outer belts can be<br />

considered for satellites in eccentric orbits. FLUMIC can be used as a tool in its own right but is also incorporated in the<br />

DICTAT internal charging tool. FLUMIC3 will be included in a new version of DICTAT to be released shortly.<br />

Author<br />

Augmentation; Electrostatics; Environment Models; Risk; Spacecraft Charging<br />

327

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