This paper reviews the history of cryogenic fluid management technology development and infusion into both the Saturn and Centaur vehicles. Ground testing and analysis proved inadequate to demonstrate full scale performance. As a consequence flight demonstration with a full scale vehicle was required by both the Saturn and Centaur programs to build confidence that problems were addressed. However; the flight vehicles were highly limited on flight instrumentation and the flight demonstration locked-in the design without challenging the function of design elements. Projects reviewed include: the Aerobee Sounding Rocket Cryogenic Fluid Management (CFM) tests which served as a valuable stepping stone to flight demonstration and built confidence in the ability to handle hydrogen in low gravity; the Saturn IVB Fluid Management Qualification flight test; the Atlas Centaur demonstration flights to develop two burn capability; and finally the Titan Centaur two post mission flight tests.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    The Role of Flight Experiments in the Development of Cryogenic Fluid Management Technologies


    Contributors:

    Conference:

    21st Space Cryogenics Workshop ; 2005 ; Colorado Springs, CO, United States


    Publication date :

    2006-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English