22,538 research outputs found

    Electrostatic ion rocket engine Patent

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    Electron bombardment ion rocket engine with improved propellant introduction syste

    Electrostatic ion engine having a permanent magnetic circuit Patent

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    Ion engine with magnetic circuit for optimal discharg

    Experimental transient vane temperatures in a cascade for gas stream temperature cycling between 922 and 1644 K (1200 and 2500 F)

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    Experimental transient turbine vane metal temperatures were obtained from tests conducted on air-cooled vanes installed in a four-vane cascade for a gas temperature cycled between 922 and 1644 K (1200 and 2500 F). Transient data were recorded by a high-speed data acquisition system. Temperatures at the same phase of each transient cycle were repeatable between cycles to within 11 kelvins (20 F), simulated cruise and idle steady-state readings were repeated by the cruise and idle readings taken from the ends of a transient half-cycle at low pressure to within 17 kelvins (30 F). The tests were conducted at pressure levels of 31 and 83 N-sq cm (45 and 120 psia) with coolant temperatures of 811 and 589 K (1000 and 600 F), respectively

    Technology utilization workshop subjects study, supplement 1

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    Aerospace technology utilization and information dissemination for industry and commerc

    Technology utilization review and analysis, Volume I Final report, 28 Feb. - 31 Aug. 1964

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    Technology utilization review and analysis of Ranger Block III program - protein detection, biochemical battery, and solar cell technolog

    Plane wave scattering from a rough surface with correlated large and small scale orders of roughness

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    Plane wave scattering from rough surface with correlated large and small scale orders of roughnes

    Maxometers (peak wind speed anemometers)

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    An instrument for measuring peak wind speeds under severe environmental conditions is described, comprising an elongated cylinder housed in an outer casing. The cylinder contains a piston attached to a longitudinally movable guided rod having a pressure disk mounted on one projecting end. Wind pressure against the pressure disk depresses the movable rod. When the wind reaches its maximum speed, the rod is locked by a ball clutch mechanism in the position of maximum inward movement. Thereafter maximum wind speed or pressure readings may be taken from calibrated indexing means
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