This paper presents a statistical evaluation of measured random vibration response data obtained from the Office of Space Science-1 (OSS-1) pallet payload. The data were measured during the acoustic test simulation (September 1980) and the ascent phase of the flight of STS-3, Orbiter 102 (launched from the Kennedy Space Center on March 22, 1982). Acoustic test efficiency factors are evaluated based on the Dynamic, Acoustic and Thermal Environments (DATE) instrumentation as the source of the measured vibration data. Test efficiency correction to test data is applied in the extrapolation of non-DATE acoustic test data to increase sample population size for improved statistical evaluation. For baseline criteria evaluation and development, data...
Acoustic data inside the payload bay and over the exterior of the orbiter were collected. The data w...
The space shuttle payload bay environment data relating to vibroacoustics and electromagnetic effect...
This report discusses the purpose and effect of environmental testing, particularly vibration, shock...
A comparative evaluation of the Space Transportation System (STS)-3 flight and acoustic test random ...
This report presents the results of a statistical analysis and evaluation performed by the Mechanica...
Data measurement and interpretation techniques were defined for application to the first few space s...
Results are presented of a research task to evaluate structural responses at various subsystem mount...
A comparative evaluation of shuttle liftoff and ground test random response data obtained from the O...
This paper presents a deterministic theory for the random vibration problem for predicting the respo...
Calculation methods for vibration responses of spacecraft structural members to acoustic field
A method of predicting broadband random vibration criteria for components on space vehicles is prese...
During liftoff and ascent flight phases, the Space Transportation System (STS) and payloads are expo...
Test methods were evaluated to ascertain whether a spacecraft, properly tested within its shroud, co...
Space average sound pressure levels computed from measurements at 18 locations in the payload bay of...
Aerospace payloads, such as satellites, are subjected to vibroacoustic excitation during launch. San...
Acoustic data inside the payload bay and over the exterior of the orbiter were collected. The data w...
The space shuttle payload bay environment data relating to vibroacoustics and electromagnetic effect...
This report discusses the purpose and effect of environmental testing, particularly vibration, shock...
A comparative evaluation of the Space Transportation System (STS)-3 flight and acoustic test random ...
This report presents the results of a statistical analysis and evaluation performed by the Mechanica...
Data measurement and interpretation techniques were defined for application to the first few space s...
Results are presented of a research task to evaluate structural responses at various subsystem mount...
A comparative evaluation of shuttle liftoff and ground test random response data obtained from the O...
This paper presents a deterministic theory for the random vibration problem for predicting the respo...
Calculation methods for vibration responses of spacecraft structural members to acoustic field
A method of predicting broadband random vibration criteria for components on space vehicles is prese...
During liftoff and ascent flight phases, the Space Transportation System (STS) and payloads are expo...
Test methods were evaluated to ascertain whether a spacecraft, properly tested within its shroud, co...
Space average sound pressure levels computed from measurements at 18 locations in the payload bay of...
Aerospace payloads, such as satellites, are subjected to vibroacoustic excitation during launch. San...
Acoustic data inside the payload bay and over the exterior of the orbiter were collected. The data w...
The space shuttle payload bay environment data relating to vibroacoustics and electromagnetic effect...
This report discusses the purpose and effect of environmental testing, particularly vibration, shock...