The digital program TBAP has been developed to provide thermal boundaries in the DD/M-relative velocity (D-V), dynamic pressure-relative velocity (q-V), and altitude-relative velocity (h-V) planes. These thermal boundaries are used to design and/or analyze shuttle orbiter entry trajectories. The TBAP has been used extensively in supporting the Flight Performance Branch of NASA in evaluating candidate trajectories for the thermal protection system design trajectory. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Thermal Boundaries Analysis Program Document


    Contributors:
    M. E. Evans (author)

    Publication date :

    1975


    Size :

    51 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Software Document Inventory Program

    Merwarth, P. D. | NTRS | 1984



    Review of Document Structure for Flight Data Analysis Program

    Zheng, Lin Lin ;Yao, Dong Lin | Trans Tech Publications | 2014