This report presents the tests results of a series of tests made of the sprays from 14 fuel injection nozzles of 9 different types, the sprays being injected into air at atmospheric density and at 6 and 14 times atmospheric density. High-speed spark photographs of the sprays from each nozzle at each air density were taken at the rate of 2,000 per second, and from them were obtained the dimensions of the sprays and the rates of spray-tip penetration. The sprays were also injected against plasticine targets placed at different distances from the nozzles, and the impressions made in the plasticine were used as an indication of the distribution of the fuel within the spray. Cross-sectional sketches of the different types of sprays are given sho...
The adiabatic half passage experiment was used to measure the rates of proton exchange reactions i...
Flow through pump components, such as the SSME-HPFTP Impeller and an advanced rocket pump impeller, ...
The effect of a leading edge flap on the aerodynamics of a low aspect ratio delta wing is studied an...
A brackish water plume rising from a submarine spring was mapped using a 192 kHz acoustic sounder an...
Transport mechanisms of zinc atoms in molten zinc were investigated by radiotracer techniques in uni...
Graphical data is presented for Type 1 ballistic transfers to Jupiter (1974 to 1986), Saturn (1976 t...
The top level, time-phased total space program support system architecture is described including pr...
The effects of potential impurities such as Na, K, Mg, Ca, and Cl, in coal-derived liquid fuels on a...
Charge efficiencies were determined by measurements made under widely differing conditions of temper...
Measurements using a balloon-borne ionization spectrometer on the differential energy spectra of the...
We present a description of the data reduction and mapmaking pipeline used for the 2008 observing se...
Spacecraft systems (fuel, electrical) are analyzed for performance prior to launch. Systems failures...
This research project was undertaken in order to determine some effective manner of enhancing the st...
Diagrams and blueprints for Guidance and Navigation (GN) & Reaction Control System (RCS) malfunction...
A simulation study to determine the 136 MHz and 400 MHz noise temperature of the ground network ante...
The adiabatic half passage experiment was used to measure the rates of proton exchange reactions i...
Flow through pump components, such as the SSME-HPFTP Impeller and an advanced rocket pump impeller, ...
The effect of a leading edge flap on the aerodynamics of a low aspect ratio delta wing is studied an...
A brackish water plume rising from a submarine spring was mapped using a 192 kHz acoustic sounder an...
Transport mechanisms of zinc atoms in molten zinc were investigated by radiotracer techniques in uni...
Graphical data is presented for Type 1 ballistic transfers to Jupiter (1974 to 1986), Saturn (1976 t...
The top level, time-phased total space program support system architecture is described including pr...
The effects of potential impurities such as Na, K, Mg, Ca, and Cl, in coal-derived liquid fuels on a...
Charge efficiencies were determined by measurements made under widely differing conditions of temper...
Measurements using a balloon-borne ionization spectrometer on the differential energy spectra of the...
We present a description of the data reduction and mapmaking pipeline used for the 2008 observing se...
Spacecraft systems (fuel, electrical) are analyzed for performance prior to launch. Systems failures...
This research project was undertaken in order to determine some effective manner of enhancing the st...
Diagrams and blueprints for Guidance and Navigation (GN) & Reaction Control System (RCS) malfunction...
A simulation study to determine the 136 MHz and 400 MHz noise temperature of the ground network ante...
The adiabatic half passage experiment was used to measure the rates of proton exchange reactions i...
Flow through pump components, such as the SSME-HPFTP Impeller and an advanced rocket pump impeller, ...
The effect of a leading edge flap on the aerodynamics of a low aspect ratio delta wing is studied an...