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71INES DATA DESCRIPTION N. Loiseau 1 , A. P´ erez-Calpena 1 , R. Gonz´ alez-Riestra  2

INES DATA DESCRIPTION N. Loiseau 1 , A. P´ erez-Calpena 1 , R. Gonz´ alez-Riestra 2

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Language: English - Date: 2000-12-05 06:33:16
72Chapter 3 Data Quality Flag Description For the creation of the IUE Final Archive, data quality (ν) flags are provided on a pixel-bypixel basis for the two-dimensional (2-D) photometrically corrected (LI) and geometrica

Chapter 3 Data Quality Flag Description For the creation of the IUE Final Archive, data quality (ν) flags are provided on a pixel-bypixel basis for the two-dimensional (2-D) photometrically corrected (LI) and geometrica

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Language: English - Date: 2000-12-05 06:33:17
73Chapter 11 Calibration of the Net Flux 11.1 Low-Dispersion Absolute Flux Calibration

Chapter 11 Calibration of the Net Flux 11.1 Low-Dispersion Absolute Flux Calibration

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Language: English - Date: 2000-12-05 06:33:18
    74INES NOISE MODEL N. Schartel1 , P. Rodr´ıguez-Pascual1,2 ESA IUE Observatory, Apartado 50727, 28080 Madrid, Spain Affiliated with the Astrophysics Division, Space Science Department ESTEC, the Netherlands 2

    INES NOISE MODEL N. Schartel1 , P. Rodr´ıguez-Pascual1,2 ESA IUE Observatory, Apartado 50727, 28080 Madrid, Spain Affiliated with the Astrophysics Division, Space Science Department ESTEC, the Netherlands 2

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    Language: English - Date: 2000-12-05 06:33:19
    75[removed]Power Subsystem. The power subsystem on the IUE spacecraft is a direct energy transfer (DET) system. The primary source of power is the spacecraft solar array which consists of two deployable paddles mounted to

    [removed]Power Subsystem. The power subsystem on the IUE spacecraft is a direct energy transfer (DET) system. The primary source of power is the spacecraft solar array which consists of two deployable paddles mounted to

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    Language: English - Date: 2000-12-05 06:33:19
    763  2. General spacecraft description. The IUE spacecraft is shown in mission orbit configuration and in an exploded view in figures 2-1 and 2-2 respectively.

    3 2. General spacecraft description. The IUE spacecraft is shown in mission orbit configuration and in an exploded view in figures 2-1 and 2-2 respectively.

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    77COMPARISON OF IUE FLUX EXTRACTION BY INES AND NEWSIPS N. Schartel1,2 , I. Skillen3 1 ESA IUE Observatory, Apartado 50727, 28080 Madrid, Spain 2

    COMPARISON OF IUE FLUX EXTRACTION BY INES AND NEWSIPS N. Schartel1,2 , I. Skillen3 1 ESA IUE Observatory, Apartado 50727, 28080 Madrid, Spain 2

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    78Appendix B Glossary The following is a list of acronyms and abbreviations used in the text of this document, along with the corresponding definitions: 1-D – 1-Dimensional 2-D – 2-Dimensional

    Appendix B Glossary The following is a list of acronyms and abbreviations used in the text of this document, along with the corresponding definitions: 1-D – 1-Dimensional 2-D – 2-Dimensional

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    Language: English - Date: 2000-12-05 06:33:18
    79THE IUE FLUX SCALE R. Gonz´ alez-Riestra Universidad Europea de Madrid, 28670 Madrid, Spain  Abstract

    THE IUE FLUX SCALE R. Gonz´ alez-Riestra Universidad Europea de Madrid, 28670 Madrid, Spain Abstract

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    Language: English - Date: 2000-12-05 06:33:16
    80[removed]Communications Subsystem. The communications system consists of two redundant VHF transponder systems, two redundant S-band transmitters with four S-band power amplifiers, and associated antenna systems. The com

    [removed]Communications Subsystem. The communications system consists of two redundant VHF transponder systems, two redundant S-band transmitters with four S-band power amplifiers, and associated antenna systems. The com

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    Source URL: godot.u-strasbg.fr

    Language: English - Date: 2000-12-05 06:33:19