Propellant condensation on surfaces near an electric rocket exhaust.
Propellant condensation on surfaces near electric rocket exhaust, calculating particle arrival rates, backflow and desorption energies
Reynolds, T. W.↗
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Propellant condensation on surfaces near an electric rocket exhaust
Propellant condensation on surfaces near electric rocket exhaust, calculating particle arrival rates, backflow and desorption energies
Reynolds, T. W.↗
Spectral radiance measurements of model rocket exhaust gases at simulated altitude, using a rapid scanning spectrometer.
Spectral radiance of model rocket exhaust gases measured by rapid scanning spectrometer at simulated altitude
EXHAUST GAS↗
Rocket exhaust effects on radio frequency transmission.
RF transmission through plasmas created by rocket exhaust of Saturn vehicle
SATURN LAUNCH VEHICLE↗
Rocket exhaust effects on radio frequency transmission.
RF transmission through plasmas created by rocket exhaust of Saturn vehicle
RADIO TRANSMISSION↗
Electrostatic rocket exhaust effects on solar- electric spacecraft subsystems.
Electrostatic rocket exhaust condensation on spacecraft solar electric panels cover glasses, noting deleterious effects
Hall, D. F.↗
Electrostatic rocket exhaust effects on solar- electric spacecraft subsystems
Electrostatic rocket exhaust condensation on spacecraft solar electric panels cover glasses, noting deleterious effects
Hall, D. F.↗
Experimental research in the use of electrets in measuring effluents from rocket exhaust and a review of standard air quality measuring devices
Seven standard types of measuring devices used to obtain the chemical composition of rocket exhaust effluents were discussed. The electrets, a new measuring device, are investigated and compared with established measuring techniques. The preliminary results obtained show that electrets have multipollutant measuring capabilities, simplicity of deployment, speed of assessment or analysis, and may be an important and valuable tool in measuring pollutants from space vehicle rocket exhaust.
Susko, M.↗
Solid-Propellant Rocket Exhaust Effects /SPREE/ and methods of attenuation, volume I - Project summary
Solid propellant rocket exhaust effects and methods of attenuation - project summary
SOLID PROPELLANT ROCKET ENGINE↗
Thermal and chemi-ionization processes in afterburning rocket exhausts.
Mathematical model for thermal and chemi- ionization processes in turbulent nonequilibrium afterburning rocket exhausts plume, studying neutral and charged species distribution
DENSITY DISTRIBUTION↗
Prediction of electron density in rocket exhaust plumes
Analytical methods of predicting electron density in rocket exhaust plumes based on detailed descriptions of flow regimes and chemical models
Audeh, B. J.↗
Analysis of the impingement of condensed rocket exhaust products upon proximate space vehicles
Impingement of condensed rocket exhaust gases upon proximate space vehicles
Wrobel, J. R.↗
Investigation of heat transfer and pressure on flat plates and curved panels due to rocket exhaust impingement
Pressures and heat transfer rate predictions for rocket exhaust impingement on flat plates and curved panels
Kooker, D. E.↗
Gas mixtures for dynamic simulation of rocket exhaust jets Final progress report, 12 Apr. - 11 Nov. 1965
Screening and evaluation of gas mixture for dynamic simulation of rocket exhaust jets
GAS MIXTURE↗
Secondary flow rates in a vertical diffuser of decreasing length using a rocket exhaust jet as the motive fluid
Secondary water flow rates in vertical diffuser of decreasing length using rocket exhaust jet as motive fluid - model sound compressor
WATER FLOW↗
Effects of impingement of rocket exhaust gases and solid particles on a spacecraft Interim report, Mar. 18 - Oct. 25, 1966
Impingement damage to spacecraft from rocket exhaust gases and micron sized metal particles
IMPINGEMENT↗
A short-duration technique for simulated rocket exhaust and wind tunnel flow and its application to the study of scale effect of recirculating flow fields.
Short duration simulation of rocket exhaust products, flow duration through nozzle and effect on recirculation flow fields
FLOW FIELD↗
Application of moderate resolution band models to the prediction of heat transfer from rocket exhaust plumes
Computer program for resolution band model prediction of heat transfer from rocket exhaust plumes
Mc Kay, G. B.↗