Performance Evaluation of Atmospheric Density Models for Satellite Reentry Predictions with High Solar Activity Levels (Articolo in rivista)

Type

• Prodotto della ricerca (Classe)
• Articolo in rivista (Classe)

Label

• Performance Evaluation of Atmospheric Density Models for Satellite Reentry Predictions with High Solar Activity Levels (Articolo in rivista) (literal)

Anno

• 2003-01-01T00:00:00+01:00 (literal)

Alternative label

• Pardini C. 1, Anselmo L. 2 (2003)
  Performance Evaluation of Atmospheric Density Models for Satellite Reentry Predictions with High Solar Activity Levels
  in Transactions of the Japan Society for Aeronautical and Space Sciences
  (literal)

Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#autori

• Pardini C. 1, Anselmo L. 2 (literal)

Pagina inizio

• 42 (literal)

Pagina fine

• 46 (literal)

Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#numeroVolume

• 46 (literal)

Rivista

• Transactions of the Japan Society for Aeronautical and Space Sciences (Rivista)

Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#note

• n. 151, May 2003 A0-25 (literal)

Note

• ISI Web of Science (WOS) (literal)

Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#affiliazioni

• 1 CNR-ISTI, 2 CNR-ISTI (literal)

Titolo

• Performance Evaluation of Atmospheric Density Models for Satellite Reentry Predictions with High Solar Activity Levels (literal)

Abstract

• In order to estimate the intrinsic accuracy of satellite reentry predictions, the residual lifetimes of eleven spacecraft and five rocket bodies, covering a broad range of inclinations and decaying from orbit in a period of high solar activity, were determined using three different atmospheric density models: JR-71, TD-88 and MSIS-86. For each object, the ballistic coefficient applicable to a specific phase of the flight was obtained by fitting an appropriate set of two-line orbital elements, while the reentry predictions were computed approximately one month, one week and one day before the final orbital decay. No clear correlation between the residual lifetime errors and the satellite inclination or type (spacecraft or rocket body) emerged. JR-71 and MSIS-86 resulted in good agreement, with comparable reentry prediction errors (~10%), semimajor axis residuals and ballistic coefficient estimations. TD-88 exhibited a behaviour consistent with the other two models, but was typically characterised by larger reentry prediction errors (~15-25%) and semimajor axis residuals. At low altitudes ( 250 km) TD-88 systematically overestimated the average atmosphere density (by ~25%) with respect to the other two models. (literal)

Prodotto di

• Istituto di scienza e tecnologie dell'informazione \"Alessandro Faedo\" (ISTI) (Istituto)

Autore CNR

• CARMEN PARDINI (Unità di personale interno)
• LUCIANO ANSELMO (Unità di personale interno)

Insieme di parole chiave

• Parole chiave di "Performance Evaluation of Atmospheric Density Models for Satellite Reentry Predictions with High Solar Activity Levels" (Insieme di parole chiave)

Incoming links:

Prodotto

• Istituto di scienza e tecnologie dell'informazione \"Alessandro Faedo\" (ISTI) (Istituto)

Autore CNR di

• CARMEN PARDINI (Unità di personale interno)
• LUCIANO ANSELMO (Unità di personale interno)

Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#rivistaDi

• Transactions of the Japan Society for Aeronautical and Space Sciences (Rivista)

Insieme di parole chiave di

• Parole chiave di "Performance Evaluation of Atmospheric Density Models for Satellite Reentry Predictions with High Solar Activity Levels" (Insieme di parole chiave)