The forward bipod system provides a robust attachment between the Space Shuttle Orbiter and the External Tank. Closed-form analyses were performed to determine how much additional load-carrying capability exists in this system beyond the current certified load limits. Results of these analyses suggest that the forward bipod system is capable of carrying loads that are at least 25 percent greater than the current flight limit loads, and possibly even more if lower safety factors are allowed. The forward bipod system may also have additional load-carrying capabilities, given the conservative nature of these analyses.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Space Shuttle Orbiter-External Tank Forward Bipod Loads Analysis


    Contributors:
    C. Wu (author)

    Publication date :

    2024


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Space Shuttle Orbiter Landing Loads Optimization

    Purtle, L. / Fann, C. / Eich, P. et al. | British Library Conference Proceedings | 1995


    Space Shuttle Orbiter landing loads optimization

    Purtle, L.V. / Fann, C.P. / Eich, P.G. | Tema Archive | 1995



    Drive Mechanism for the Shuttle Orbiter/External Tank Propellant Disconnect

    E. Thomas / R. Wilders / J. Ulanovsky | NTRS | 1981


    Space Shuttle External Tank.

    Zoller, L. K. | NTRS | 1973