The development of the thermal protection system for the Solid Rocket Booster is reported. Tests and analytical efforts were conducted and new problems are continually attacked and solved. During the first six Shuttle flights it was necessary to make a final thermal assessment of the TPS and structural systems temperatures. The thermal assessments were made and are compared with post flight data.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Shuttle SRB Preflight/Post-Flight Thermal Assessment


    Publication date :

    1985


    Size :

    9 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English