Assessment of available IR sensor technology showed that the four aerothermodynamic conditions of interest during the entry trajectory of space shuttle can be accommodated by an aircraft flying parallel to the orbiter reentry ground track. Thermal information from the sides of the vehicle can be obtained with degraded performance (temperatures below 800 K) by flying the C-141 aircraft on the opposite side of the shuttle ground track and in the direction opposite that which is optimum for lower surface viewing. An acquisition system using a 6.25-cm aperture telescope and a single indium antimonide detector were designed to meet the acquisition requirements and interface with the 91.5-cm telescope with minimum modification. An image plane system using 600 indium antimonide detectors in two arrays which requires no modification to the existing telescope was also designed. Currently available components were used in a data handling system with interfaces with the experimentors station and the HP2100 computer.


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    Titel :

    Infrared Imagery of Shuttle (IRIS). Task 1


    Beteiligte:
    C. J. Chocol (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    151 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    Remote infrared imagery of shuttle during entry

    Chocol, C.J. | Tema Archiv | 1979


    Infrared Imagery of the Space Shuttle at Hypersonic Entry Conditions

    Ross, M. / Werner, M. / Mazuk, S. et al. | British Library Conference Proceedings | 2008