44,852 research outputs found

    Decay of Z into Three Pseudoscalar Bosons

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    We consider the decay of the ZZ boson into three pseudoscalar bosons in a general two-Higgs-doublet model. Assuming mAm_A to be very small, and that of the two physical neutral scalar bosons h1h_1 and h2h_2, AA only couples to ZZ through h1h_1, we find the ZAAAZ \to A A A branching fraction to be negligible for moderate values of tanβv2/v1\tan \beta \equiv v_2/v_1, if there is no λ5(Φ1Φ2)2+h.c.\lambda_5 (\Phi_1^\dagger \Phi_2)^2 + h.c. term in the Higgs potential; otherwise there is no absolute bound but very large quartic couplings (beyond the validity of perturbation theory) are needed for it to be observable.Comment: 8 pages including 1 fi

    How to Use a Business Library

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    Speech delivered on the Bryant\u27s View radio program by Miss Dorothy E. Keith, Bryant College Librarian, on the Bryant\u27s View radio program, Thursday, May 10, 1956, Station WPRO

    Seeding of Strange Matter with New Physics

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    At greater than nuclear densities, matter may convert into a mixture of nucleons, hyperons, dibaryons, and strangelets, thus facilitating the formation of strange matter even before the onset of the quark-matter phase transition. From a nonstrange dibaryon condensate, it may even be possible to leapfrog into strange matter with a certain new interaction, represented by an effective six-quark operator which is phenomenologically unconstrained.Comment: 7 pages, no figure (Talk given at SQM97

    OMV mission simulator

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    The Orbital Maneuvering Vehicle (OMV) will be remotely piloted during rendezvous, docking, or proximity operations with target spacecraft from a ground control console (GCC). The real-time mission simulator and graphics being used to design a console pilot-machine interface are discussed. A real-time orbital dynamics simulator drives the visual displays. The dynamics simulator includes a J2 oblate earth gravity model and a generalized 1962 rotating atmospheric and drag model. The simulator also provides a variable-length communication delay to represent use of the Tracking and Data Relay Satellite System (TDRSS) and NASA Communications (NASCOM). Input parameter files determine the graphics display. This feature allows rapid prototyping since displays can be easily modified from pilot recommendations. A series of pilot reviews are being held to determine an effective pilot-machine interface. Pilots fly missions with nominal to 3-sigma dispersions in translational or rotational axes. Console dimensions, switch type and layout, hand controllers, and graphic interfaces are evaluated by the pilots and the GCC simulator is modified for subsequent runs. Initial results indicate a pilot preference for analog versus digital displays and for two 3-degree-of-freedom hand controllers
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