Experimental and theoretical investigation of plasma radiation Semiannual status report, Sep. 1969 - Feb. 1970
Stark broadening of argon and neon resonance lines
Greig, J. R.↗
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Results for “neon”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Rotational excitations of molecules by collision with atoms
Rotational excitation cross sections of nitrogen by neon impact
Faisal, F. H. M.↗
Elastic and inelastic scattering of 18-MeV protons on Ne 20
Cross section scattering and polarization data of 18 MeV protons from neon 20
Baron, N.↗
The polarization of Lyman alpha radiation produced in charge transfer collisions between protons and the inert gases
Polarization of Lyman alpha radiation in proton collisions with helium, argon, and neon atoms
Fite, W. L.↗
Research directed toward perfecting a design for a space qualified He-Ne laser, phase 2
Helium-neon laser and power supply for spacecraft
Kolb, W. P.↗
Electron temperature dependence of recombination of Ne super plus sub 2 ions with electrons
Electron temperature dependence of molecular neon ions recombination with electrons using microwave afterglow/mass spectrometer, obtaining recombination coefficient
Biondi, M. A.↗
Line strengths and radiative lifetimes for Ne II
Line strength and radiative lifetimes for Ne II determined from spontaneous emission data obtained from CW neon laser discharge
Hodges, D.↗
Design for a space qualified laser, phase 1
Design for space qualified helium-neon laser
Bridges, W. B.↗
Investigation of intermittent enhancement of ion emission from a tungsten surface using the field ion microscope
Measuring intermittent enhancement of blinking effect upon addition of neon to imaging gas in helium-tungsten field-ion microscope
Weizer, V. G.↗
Development and endurance testing of high- temperature ceramic voltage-regulator tubes
Long-term performance tests of neon gas filled, high-temperature ceramic voltage-regulator tubes
Jones, N. D.↗
Electron bombardment ion source operation using various gases
Space electric rocket test thruster performance with xenon, krypton, argon, neon, nitrogen, helium, and carbon dioxide ion source gases and magnetic spectroscopy of ion emissions
Byers, D. C.↗
Experimental investigations of optical propagation in atmospheric turbulence
Analysis of helium-neon and carbon dioxide laser beam propagation in atmospheric turbulence
Fitzmaurice, M. W.↗
Density and flux distributions of neutral gases in the lunar atmosphere
Neon, argon, and helium density and flux distributions in lunar atmosphere
Yeh, T. T. J.↗
Inelastic scattering calculations with projected Hartree-Fock wave functions: Coupled channel treatment
Microscopic coupled-channel analysis of proton inelastic scattering from neon and magnesium ions
Ascuitto, R. J.↗
Electron-bombardment ion source operation using various gases
Performance tests of electron bombardment ion thrustor, using xenon, krypton argon, neon, nitrogen, helium and carbon dioxide
Byers, D. C.↗
Lunar atmosphere
Lunar atmospheric contributions from solar wind, meteoric volatilization, internal degassing and rocket gases, discussing day and night neon concentrations
Johnson, F. S.↗
New reaction tester accurate within 56 microseconds
Testing device measures simple and disjunctive reaction time of human subject to light stimuli. Tester consists of reaction key, logic card, panel mounted neon indicators, and interconnecting wiring. Device is used for determining reaction times of patients undergoing postoperative neurological therapy.
Brown, H.↗
A general stagnation-point convective heating equation for arbitrary gas mixtures
The stagnation-point convective heat transfer to an axisymmetric blunt body for arbitrary gases in chemical equilibrium was investigated. The gases considered were base gases of nitrogen, oxygen, hydrogen, helium, neon, argon, carbon dioxide, ammonia, and methane and 22 gas mixtures composed of the base gases. Enthalpies ranged from 2.3 to 116.2 MJ/kg, pressures ranged from 0.001 to 100 atmospheres, and the wall temperatures were 300 and 1111 K. A general equation for the stagnation-point convective heat transfer in base gases and gas mixtures was derived and is a function of the mass fraction, the molecular weight, and a transport parameter of the base gases. The relation compares well with present boundary-layer computer results and with other analytical and experimental results. In addition, the analysis verified that the convective heat transfer in gas mixtures can be determined from a summation relation involving the heat transfer coefficients of the base gases. The basic technique developed for the prediction of stagnation-point convective heating to an axisymmetric blunt body could be applied to other heat transfer problems.
Sutton, K.↗