Test operations of the Scanning Laser Doppler System (SLDS) at Kennedy International Airport (KIA) during August 1974 through June 1975 are reported. A total of 1,619 data runs was recorded with a totally operational system during normal landing operations at KIA. In addition, 53 data runs were made during cooperative flybys with the C880 for a grand total of 1672 recorded vortex tracks. Test crews were in attendance at KIA for 31 weeks, of which 25 weeks were considered operational and the other six were packing, unpacking, setup and check out. Although average activity equates to 67 recorded landing operations per week, two periods of complete runway inactivity spanned 20 days and 13 days, respectively. The operation frequency therefore a...
The demand of more powerful tools for remote sensing and management of earth resources steadily incr...
A study task is reported which is directed towards developing a conceptual design of a small, lightw...
Supersonic aerodynamic tests were conducted in the NASA/LaRC Unitary Plan Wind Tunnel on a 0.015-sca...
The first detailed velocity profile data on thermally induced dust vortices are presented. These dus...
The author had identified the following significant results. Repeated looks at surfaces that maintai...
The features of the microburst on August 2, 1985, related to the Delta 191 accident during the appro...
An Earth Resources Data Processing System was developed to evaluate the system for training, technol...
The system control and signal conditioning electronics of the NASA three laser airborne differential...
In 1982 a workshop was held to refine the science rationale for large deployable reflectors (LDR) an...
A simulation program which provided information on theoretically expected vortex spectra, evaluation...
The proximity translation and final docking of the space teleoperator evaluation vehicle (STEV) with...
A series of microwave measurements was conducted to determine the radar cross section of the Space S...
A flight test program was conducted in which the effects of various surface coatings on aerodynamic ...
An overall introduction to the NASA sounding rocket program as managed by the Goddard Space Flight C...
Calibration method and ultrahigh vacuum components for ionization gage and mass spectromete
The demand of more powerful tools for remote sensing and management of earth resources steadily incr...
A study task is reported which is directed towards developing a conceptual design of a small, lightw...
Supersonic aerodynamic tests were conducted in the NASA/LaRC Unitary Plan Wind Tunnel on a 0.015-sca...
The first detailed velocity profile data on thermally induced dust vortices are presented. These dus...
The author had identified the following significant results. Repeated looks at surfaces that maintai...
The features of the microburst on August 2, 1985, related to the Delta 191 accident during the appro...
An Earth Resources Data Processing System was developed to evaluate the system for training, technol...
The system control and signal conditioning electronics of the NASA three laser airborne differential...
In 1982 a workshop was held to refine the science rationale for large deployable reflectors (LDR) an...
A simulation program which provided information on theoretically expected vortex spectra, evaluation...
The proximity translation and final docking of the space teleoperator evaluation vehicle (STEV) with...
A series of microwave measurements was conducted to determine the radar cross section of the Space S...
A flight test program was conducted in which the effects of various surface coatings on aerodynamic ...
An overall introduction to the NASA sounding rocket program as managed by the Goddard Space Flight C...
Calibration method and ultrahigh vacuum components for ionization gage and mass spectromete
The demand of more powerful tools for remote sensing and management of earth resources steadily incr...
A study task is reported which is directed towards developing a conceptual design of a small, lightw...
Supersonic aerodynamic tests were conducted in the NASA/LaRC Unitary Plan Wind Tunnel on a 0.015-sca...