41,020 research outputs found

    Design evolution of a low shock release nut

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    Design improvements and detailed functional analyses are reviewed to trace the development of a pyroactuated release device with segmented thread design from its intermediate design into one that reduces the levels of shock spectra generated during its operation by 50%. Comparisons of shock output and internal load distribution are presented, along with descriptions of mechanical operation for both designs. Results also show the potential areas where design development activity can gain further progress in lowering actuation shock levels

    Measuring the Efficiency Cost of Taxing Risky Capital Income

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    In this paper, we derive a measure of the efficiency cost of taxing risky capital income in an infinite horizon stochastic model. The resulting measure differs from all those that have been proposed in the existing literature. It can be represented by the expression -sigma(s) T(s)c(deltaX(s)), where T(s) measures the present value of the taxes that would be paid on a unit of investment in a riskless project with the same expected depreciation rate and tax treatment as capital invested in period s, X(s), while c(X(s)) represents the certainty equivalent to the representative individual of the lottery where measures the ex post change in investment in period s due to the tax change. The paper then compares this measure with others that have appeared in the literature. We were unable to find support for the argument in Bulow-Suinmers(1984) that the efficiency cost of taxing risky capital income is much larger than that implied by the measure -sigma(s)T(s)E(deltaX(s)). In fact, we show in special cases that our measure implies a smaller efficiency cost than does the measure -sigma(s)T(s)E(deltaX(s)).

    Transport in ultradilute solutions of 3^3He in superfluid 4^4He

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    We calculate the effect of a heat current on transporting 3^3He dissolved in superfluid 4^4He at ultralow concentration, as will be utilized in a proposed experimental search for the electric dipole moment of the neutron (nEDM). In this experiment, a phonon wind will generated to drive (partly depolarized) 3^3He down a long pipe. In the regime of 3^3He concentrations <~109\tilde < 10^{-9} and temperatures 0.5\sim 0.5 K, the phonons comprising the heat current are kept in a flowing local equilibrium by small angle phonon-phonon scattering, while they transfer momentum to the walls via the 4^4He first viscosity. On the other hand, the phonon wind drives the 3^3He out of local equilibrium via phonon-3^3He scattering. For temperatures below 0.50.5 K, both the phonon and 3^3He mean free paths can reach the centimeter scale, and we calculate the effects on the transport coefficients. We derive the relevant transport coefficients, the phonon thermal conductivity and the 3^3He diffusion constants from the Boltzmann equation. We calculate the effect of scattering from the walls of the pipe and show that it may be characterized by the average distance from points inside the pipe to the walls. The temporal evolution of the spatial distribution of the 3^3He atoms is determined by the time dependent 3^3He diffusion equation, which describes the competition between advection by the phonon wind and 3^3He diffusion. As a consequence of the thermal diffusivity being small compared with the 3^3He diffusivity, the scale height of the final 3^3He distribution is much smaller than that of the temperature gradient. We present exact solutions of the time dependent temperature and 3^3He distributions in terms of a complete set of normal modes.Comment: NORDITA PREPRINT 2015-37, 9 pages, 6 figure

    Tax Structure and Government Behavior: Implications for Tax Policy

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    Changes in tax policy can affect all aspects of the economy. Not only do firms and individuals change behavior, creating efficiency costs, but government expenditure choices can also change. Unless these expenditure choices had been optimal' previously, changes in response to a tax reform affect welfare and should be taken into account when designing tax policy. This paper develops a specific model of government behavior and then explores the implications of government, as well as private, behavioral responses for tax policy. In particular, we assume that government officials favor expenditure (or regulatory) choices that increase the government's budget. As a result, higher tax rates on a particular activity encourage government behavior that aids the growth of this activity. This response enables tax policy to redirect government activity in desirable directions, but it also makes Pigovian taxes on negative externalities less effective.

    Low Temperature Transport Properties of Very Dilute Classical Solutions of 3^3He in Superfluid 4^4He

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    We report microscopic calculations of the thermal conductivity, diffusion constant and thermal diffusion constant for classical solutions of 3^3He in superfluid 4^4He at temperatures T \la 0.6~K, where phonons are the dominant excitations of the 4^4He. We focus on solutions with 3^3He concentrations \la \,10^{-3}, for which the main scattering mechanisms are phonon-phonon scattering via 3-phonon Landau and Beliaev processes, which maintain the phonons in a drifting equilibrium distribution, and the slower process of 3^3He-phonon scattering, which is crucial for determining the 3^3He distribution function in transport. We use the fact that the relative changes in the energy and momentum of a 3^3He atom in a collision with a phonon are small to derive a Fokker-Planck equation for the 3^3He distribution function, which we show has an analytical solution in terms of Sonine polynomials. We also calculate the corrections to the Fokker-Planck results for the transport coefficients.Comment: 29 pages, 2 figure

    Transport in very dilute solutions of 3^3He in superfluid 4^4 He

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    Motivated by a proposed experimental search for the electric dipole moment of the neutron (nEDM) utilizing neutron-3^3He capture in a dilute solution of 3^3He in superfluid 4^4 He, we derive the transport properties of dilute solutions in the regime where the 3^3He are classically distributed and rapid 3^3He-3^3He scatterings keep the 3^3He in equilibrium. Our microscopic framework takes into account phonon-phonon, phonon-3^3He, and 3^3He-3^3He scatterings. We then apply these calculations to measurements by Rosenbaum et al. [J.Low Temp.Phys. {\bf 16}, 131 (1974)] and by Lamoreaux et al. [Europhys.Lett. {\bf 58}, 718 (2002)] of dilute solutions in the presence of a heat flow. We find satisfactory agreement of theory with the data, serving to confirm our understanding of the microscopics of the helium in the future nEDM experiment.Comment: 10 pages, 5 figures, v

    Solution of a statistical mechanics model for pulse formation in lasers

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    We present a rigorous statistical-mechanics theory of nonlinear many mode laser systems. An important example is the passively mode-locked laser that promotes pulse operation when a saturable absorber is placed in the cavity. It was shown by Gordon and Fischer [1] that pulse formation is a first-order phase transition of spontaneous ordering of modes in an effective "thermodynamic" system, in which intracavity noise level is the effective temperature. In this paper we present a rigorous solution of a model of passive mode locking. We show that the thermodynamics depends on a single parameter, and calculate exactly the mode-locking point. We find the phase diagram and calculate statistical quantities, including the dependence of the intracavity power on the gain saturation function, and finite size corrections near the transition point. We show that the thermodynamics is independent of the gain saturation mechanism and that it is correctly reproduced by a mean field calculation. The outcome is a new solvable statistical mechanics system with an unstable self-interaction accompanied by a natural global power constraint, and an exact description of an important many mode laser system.Comment: 10 pages, 3 figures, RevTe

    Midcourse maneuver operations program

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    Midcourse Maneuver Operations Program /MMOP/ computes the required velocity change to correct a spacecraft trajectory. The program establishes the existence of maneuvers which satisfy spacecraft constraints, explores alternate trajectories in the event that some out-of-tolerance condition forces a change in plans, and codes the maneuvers into commands
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