Add to ORKGThis paper presents a deterministic theory for the random vibration problem for predicting the response of structures in the low-frequency range (0 to 20 hertz) of launch transients. Also presented are some innovative ways to characterize noise and highlights of ongoing test-analysis correlation efforts titled the Verification Test Article (VETA) project
The response of reusable space shuttle insulation panels to random acoustic pressure fields are stud...
A comprehensive, automated, and user-friendly software program was developed to predict the noise an...
A high intensity acoustic test in a reverberant chamber was conducted on the CASSIOPE spacecraft in ...
This study consists of an investigation into the nonstationary transient response of the Verificatio...
The design of launch pad structures, particularly those having a large area-to-mass ratio, is govern...
Aerospace payloads, such as satellites, are subjected to vibroacoustic excitation during launch. San...
During liftoff and ascent flight phases, the Space Transportation System (STS) and payloads are expo...
Calculation methods for vibration responses of spacecraft structural members to acoustic field
This paper presents a statistical evaluation of measured random vibration response data obtained fro...
The general methodology for the analysis of arbitrary nonstationary random data is reviewed. A speci...
The liftoff phase induces some of the highest acoustic loading over a broad frequency for a launch v...
Theoretical models were developed capable of predicting structural response and noise transmission t...
A method of predicting broadband random vibration criteria for components on space vehicles is prese...
The Clementine Spacecraft was launched on January 25, 1994 from Vandenberg Air Force Base. The space...
Three major goals were delineated: (1) to develop a general method for determining the response of a...
The response of reusable space shuttle insulation panels to random acoustic pressure fields are stud...
A comprehensive, automated, and user-friendly software program was developed to predict the noise an...
A high intensity acoustic test in a reverberant chamber was conducted on the CASSIOPE spacecraft in ...
This study consists of an investigation into the nonstationary transient response of the Verificatio...
The design of launch pad structures, particularly those having a large area-to-mass ratio, is govern...
Aerospace payloads, such as satellites, are subjected to vibroacoustic excitation during launch. San...
During liftoff and ascent flight phases, the Space Transportation System (STS) and payloads are expo...
Calculation methods for vibration responses of spacecraft structural members to acoustic field
This paper presents a statistical evaluation of measured random vibration response data obtained fro...
The general methodology for the analysis of arbitrary nonstationary random data is reviewed. A speci...
The liftoff phase induces some of the highest acoustic loading over a broad frequency for a launch v...
Theoretical models were developed capable of predicting structural response and noise transmission t...
A method of predicting broadband random vibration criteria for components on space vehicles is prese...
The Clementine Spacecraft was launched on January 25, 1994 from Vandenberg Air Force Base. The space...
Three major goals were delineated: (1) to develop a general method for determining the response of a...
The response of reusable space shuttle insulation panels to random acoustic pressure fields are stud...
A comprehensive, automated, and user-friendly software program was developed to predict the noise an...
A high intensity acoustic test in a reverberant chamber was conducted on the CASSIOPE spacecraft in ...