Electron density and temperature measurements in the exhaust of an MPD source.
Electron density and temperature measured in exhaust of magnetoplasmadynamic /MPD/ source, using Langmuir probe and spectrometry
PLASMA SPECTRUM↗
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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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Investigation of the discharge and exhaust beam of a small arc plasma thrustor.
Discharge and exhaust beam of small low-power DC magnetic expansion thrustor
PLASMA PROPULSION↗
Axial current distribution in the exhaust of the magnetic annular arc.
Axial current distribution in exhaust of magnetic annular arc, examining effect of entrainment on thrust measurement
MAGNETIC ANNULAR ARC↗
Effects of aerobic work performed during recovery from exhausting work.
Oxygen debt and rate of lactate removal in physically fit men during recovery following exhausting runs on treadmill
PHYSICAL EXERCISE↗
Interaction effects of a control jet exhausting radially from the nose of an ogive- cylinder body at transonic speeds
Interaction effects of control jet exhausting radially from nose of ogive-cylinder body at transonic speeds
TRANSONIC SPEED↗
Application of Exhaust Diffusers for Rocket Engine Testing
Applications of exhaust diffusers for chemical propellant rocket engine testing
DIFFUSER↗
Axial current distribution in the exhaust of the magnetic annular arc.
Axial current distribution in exhaust of magnetic annular arc, examining effect of entrainment on thrust measurement
THRUST MEASUREMENT↗
General Computer Program for Calculation of Radiation from Inhomogeneous, Nonisobaric, Nonisothermal Rocket Exhaust Plume
Computer program evaluates radiation from an axisymmetric gas body with water vapor, carbon dioxide, carbon monoxide, and solid carbon particles as radiating constituents, and hydrogen as a nonradiating constituent. The program provides a convenient method of evaluating a great many problems of radiation from rocket exhaust plumes.
Dash, M. J.↗
Infrared spectroradiometer for rocket exhaust analysis
Infrared spectroradiometer measures high-resolution spectral absorption, emission, temperature, and concentration of chemical species in radically symmetric zones of the exhaust plumes of large rocket engines undergoing static firing tests. Measurements are made along predetermined lines of sight through the plume.
Herget, W. F.↗
Study of exhaust plume radiation predictions Final report
Methods for predicting radiative base heating by hot water vapor in rocket exhaust gases
Source record↗
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.↗
The effect of mixing, radiation, and finite rate combustion upon the flow field and surroundings of the exhaust plumes of rocket engines burning RP1 /kerosene/ and liquid oxygen
Shear layer mixing, hydrocarbon oxidation, and carbon cloud radiation models for liquid rocket engine exhaust plume analysis
Edelman, R.↗
Additional development of a probe to measure velocity distributions in the exhaust of steady state plasma accelerators Final report
Probe to measure velocity distributions in exhaust of steady-state plasma accelerators
Liebing, L.↗
NES exhaust plume scale model measurements and full scale predictions. NERVA program
Predicted full scale exhaust plume length and thermal radiation flux at proximate surfaces from scale model data
Source record↗
Appendix A - A study of contamination of Surveyor 5 landing site by main retro exhaust
Surveyor 5 landing site contamination from solid aluminum oxide particles in main retro exhaust
Franzgrote, E. J.↗
Radiative heat transfer calculations for Saturn exhaust plumes
Computer programs for predicting radiative heat transfer for Saturn exhaust plumes
Huffaker, R. M.↗
Forces and moments produced by air and helium jets exhausting parallel to a flat plate in a near vacuum
Forces and moments produced by air and helium jets exhausting parallel to flat plate in near vacuum
Hoffman, S.↗
Study of underexpanded exhaust jets of an X-15 airplane model and attached ramjet engine simulator at Mach 6.86
Approximation of ramjet exhaust plume effects on external pressure of nozzle extension of X-15 aircraft
Andrews, E. H., Jr.↗