Magnetostatic cleanliness of the radioisotope thermoelectric generators (RTGs) of Cassini

IEEE International Symposium on Electromagnetic Compatibility

Volumn 2, Issue , 1999, Pages 899-904

  Mehlem, K ^a   Narvaez, P ^b  

^a EUROPEAN SPACE AGENCY   (Netherlands)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ELECTROMAGNETIC COMPATIBILITY; ELECTROMAGNETIC PULSE; ELECTRONIC EQUIPMENT; MAGNETIC FIELDS; MAGNETISM; MAGNETOSTATICS; RADIOISOTOPES; SPACECRAFT; THERMOELECTRIC EQUIPMENT; ELECTROMAGNETIC FIELDS; MAGNETIC VARIABLES MEASUREMENT; MAGNETOMETERS; MATHEMATICAL MODELS; SATELLITES;

CASSINI; CASSINI SPACECRAFT; DC MAGNETIC FIELD; FIELD MAPPING; MAGNETIC FIELD DATA; MAGNETIC FIELD INTERFERENCE; MAGNETIC FIELD PERTURBATIONS; RADIOISOTOPE THERMOELECTRIC GENERATORS;

NUCLEAR BATTERIES; THERMOELECTRIC EQUIPMENT;

DC MAGNETIC FIELD SCIENCE INSTRUMENTS; ELECTROMAGNETIC INTERFERENCE; FIELD MAPPING TECHNIQUE; MAGNETIC FIELD INTERFERENCE; RADIOISOTOPE THERMOELECTRIC GENERATORS;

EID: 0033338620     PISSN: 10774076     EISSN: 21581118     Source Type: Conference Proceeding    
DOI: 10.1109/ISEMC.1999.810175     Document Type: Conference Paper

References (8)

1. Eichom W L 1972, Magnetic dipole moment determination by near field analysis, NASA TN D-6685, July 1972.
2. Neubauer F M 1974, Theoretical and observational analysis of spacecraft fields, J Geophys Res, April 1974.
3. Polak E 1971, Computational methods in optimization. Academic Press.
4. Mehlem K 1978, Multiple magnetic dipole modeling and field prediction of satellites, IEEE Trans on Magnetics, September 1978.
5. Mehlem K 1989, Ulysses RTG F3 magnetic compensation, ESA/ESTEC Working Paper 1537, March 1989.
6. Mehlem K 1996/97, Cassini RTG F5, F2, F7, F6 magnetic analysis report, ESA/ESTEC-JPL internal working paper, 1996/97.
7. Narvaez P 1990, RTG Impact On Magnetometer Experiment Due To New Stacked Configuration, JPL IOM 5215-90-90, internal memorandum, April 199O.
8. Narvaez P 1993, Rationale For Cassini Spacecraft RTG Self-Compensation, JPL IOM 5215-93-104, internal memorandum, March 1993.