A concept study was performed in 1994 to develop a mission design for a telescope to achieve the highest possible spatial resolution in the 10-30 micron range within a $200 million mission cost cap. The selected approach for the resulting Mid-Infrared Optimized Resolution Spacecraft (MIRORS) concept design utilizes a partially filled five meter aperture.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Mid-Infrared Optimized Resolution Spacecraft (MIRORS)


    Contributors:
    van Buren, D. (author) / Rourke, K. (author) / Hawarden, T. G. (author) / Kadogawa, H. (author) / Tereby, S. (author) / Lilienthal, G. W. (author) / Wade, L. A. (author)

    Publication date :

    1996-08-06


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Mid-InfraRed Optimized Resolution Spacecraft (MIRORS)

    Terebey, Susan / Lilienthal, Gerald W. / Kadogawa, Hiroshi et al. | NTRS | 1996


    Optimized Architecture for Passenger Spacecraft

    Adams, Constance / Petrov, Georgi / Ciardullo, Christina et al. | AIAA | 2008


    Optimized Architecture for Passenger Spacecraft

    Adams, C. / Petrov, G. / Ciardullo, C. et al. | British Library Conference Proceedings | 2008



    Optimized Relative Motion for Spacecraft Formation

    Altes Arlandis, B. / Cremaschi, F. / Schaff, S. et al. | British Library Conference Proceedings | 2008