Space storable propulsion system comparison.
Space storable propulsion system comparison, discussing liquid propellants performance and thermodynamic analysis
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Space storable propulsion system comparison, discussing liquid propellants performance and thermodynamic analysis
Paper presents mathematical comparison of several techniques with the limiting slope technique for data reduction and reconstruction. Limiting slope method results in maximum possible RMS error versus data compression ratio advantage of 2-to-1 over step and fan methods and 3-to-1 over the two point projection method.
Comparison of class of orbits in Earth-Moon field and class of Kepler orbits in rotating coordinates by use of concurrent series of graphs
Performance comparisons of supersonic compressor rotor blades
Parametric study of B-58 acceleration response to turbulence and comparisons with flight data
Comparisons of wind and temperature data obtained by Japanese MT-135 and American ARCAS meteorological rocket systems in closely spaced launchings
Comparison of ion and electron density and temperature and ionic species measurements made by Explorer 31
Theoretical comparison of beads, wires, and films as rocketsonde temperature sensors in mesosphere
Comparison of electromagnetic and centrifugal pumps for cesium and potassium Rankine cycle systems
Documentation of Explorer 32 electron temperature measurements used in comparisons with backscatter measurements at Jicamarca
Comparison and analysis between topside and ground based measurements of ionospheric electron density profiles
Comparison of extraction procedures using 1-nitroso 2-naphthol and dimethylglyoxime for spectrophotometric determination of palladium in titanium alloys
Comparison of Brayton and Rankine cycle magnetogasdynamic space power generation systems for use with nuclear heat source
Comparison of theoretical and measured orbital perturbations of artificial earth satellites
Systematic investigation of mathematical models by comparison of experimental and analytical regression coefficients
Design comparison of cesium and potassium vapor turbogenerator units for space power plants
Accuracy and speed comparison between drag-free and numerical satellite orbit prediction methods
Energy spectra comparison of cosmic ray helium and heavy nuclei