Spacecraft instrument module configurations which support an earth resource data gathering mission using a thematic mapper sensor were examined. The differences in size of these two experiments necessitated the development of two different spacecraft configurations. Following the selection of the best-suited configurations, a validation phase of design, analysis and modelling was conducted to verify feasibility. The chosen designs were then used to formulate definition for a systems weight, a cost range for fabrication and interface requirements for the thematic mapper (TM).


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Landsat D Instrument Module Study


    Publication date :

    1976


    Size :

    242 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Landsat Data Continuity Mission Expected Instrument Performance

    Dabney, Philip W. / Irons, James R. / Markham, Brian L. et al. | NTRS | 2012



    Landsat/MMS Propulsion Module Design. TAS4.4: Concept Design

    J. M. Mansfield / F. G. Etheridge / J. Indrikis | NTIS | 1976


    LANDSAT/MMS propulsion module design. Tas4.4: Concept design

    Mansfield, J. M. / Etheridge, F. G. / Indrikis, J. | NTRS | 1976