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  • April 26th - Lunch & Learn with Special Guest Dr. Albert Allen Jackson IV

    Join AIAA Houston Section for a hybrid Lunch & Learn event with special guest Dr. Albert Allen Jackson IV, on
    April
    26th, 2024 at 11:30 CST in person and over Google Meet
    dr-albert-allen
    Sign up to attend: Lunch-n-Learn Sign Up

    "The Interstellar Ramjet: A Technical History" 
    In 1960 Robert Bussard published a solution to the mass ratio problem for interstellar flight. He laid out
    the design of a starship that scooped interstellar hydrogen compressed it in a fusion reactor, extracted energy
    and produced thrust. The process is similar to a terrestrial ramjet.
    Bussard outlined the propulsion method, presented the equations of
    motion and made general assessments of performance and
    propulsion efficiency.
    Sagan suggested magnetic 'scoops' for collecting working
    matter from the interstellar medium. Fishback in 1969 calculated
    important limitations on the ramjet magnetic intake and quantified
    drag and radiation losses for the ramjet.
    Fishback showed there was a limiting Lorentz factor for an
    interstellar ramjet imposed by the material properties of the scoop
    source.
    Tony Martin expanded Fishback study and made some
    important observations. The main problem with the concept was
    using proton-proton reactions for fusion, this proves very difficult.
    In 1975 Dan Whitmire made progress towards solving the fusion reactor problem of the interstellar ramjet
    by noting that one could use the CNO process rather than the PP mechanism as method of fusion operation.
    Bond and Jackson suggested alternative ramjet operation using augmentation. An alternative to the
    Bussard Ramjet was presented in 1977. The Laser Powered Interstellar Ramjet, LPIR. This vehicle uses a
    solar system-based laser beaming power to a vehicle which scoops interstellar hydrogen and uses a linear
    accelerator to boost the collected particle energy for propulsion bypassing fusion reactor problems.



    Link:
    Or dial: (US) +1 314-474-3017 PIN: 913 841 786#
    Hope to see you there!
    AIAA Houston Section