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Compilation of shock, vibration, and acoustic data from Titan vehicles. Volume III - Titan II shock, vibration, and acoustic data
Vibration, acoustic, and shock data tabulated for Titan II ICBM
Saturn S-I-10 static test vibration and acoustic data
Vibration and sound intensity measurements of Saturn S-I-10 vehicle in static testing
Vibration and acoustics structural research
Vibration and acoustics effect on vehicle structural design
Acoustically Induced Vibration of Structures: Reverberant Vs. Direct Acoustic Testing
Large reverberant chambers have been used for several decades in the aerospace industry to test larger structures such as solar arrays and reflectors to qualify and to detect faults in the design and fabrication of spacecraft and satellites. In the past decade some companies have begun using direct near field acoustic testing, employing speakers, for qualifying larger structures. A limited test data set obtained from recent acoustic tests of the same hardware exposed to both direct and reverberant acoustic field testing has indicated some differences in the resulting structural responses. In reverberant acoustic testing, higher vibration responses were observed at lower frequencies when compared with the direct acoustic testing. In the case of direct near field acoustic testing higher vibration responses appeared to occur at higher frequencies as well. In reverberant chamber testing and direct acoustic testing, standing acoustic modes of the reverberant chamber or the speakers and spacecraft parallel surfaces can strongly couple with the fundamental structural modes of the test hardware. In this paper data from recent acoustic testing of flight hardware, that yielded evidence of acoustic standing wave coupling with structural responses, are discussed in some detail. Convincing evidence of the acoustic standing wave/structural coupling phenomenon will be discussed, citing observations from acoustic testing of a simple aluminum plate. The implications of such acoustic coupling to testing of sensitive flight hardware will be discussed. The results discussed in this paper reveal issues with over or under testing of flight hardware that could pose unanticipated structural and flight qualification issues. Therefore, it is of paramount importance to understand the structural modal coupling with standing acoustic waves that has been observed in both methods of acoustic testing. This study will assist the community to choose an appropriate testing method and test setup in the planning stages.
Vibration and acoustic analyses, Saturn SA-10 flight
Vibration and acoustic analysis Saturn SA-10 FLIGHT
A telemetry standard for vibration and acoustic measurements
Telemetry standard for vibration and acoustic measurements
Random-vibration response data for orbiting geophysical observatory - Flight, acoustic, and vibration test
Random vibration response data for orbiting geophysical observatory - comparative analysis of flight, acoustic, and vibration tests
Design of space vehicle structures for vibration and acoustic environments
Space vehicle structures for vibration and acoustic environment
Study to define Agena vibration and acoustic environment
Acoustic excitation and random vibration measurements for Agena vehicle
Summary of vibration and acoustic tests on four spacecraft programs
Vibration and acoustic tests on Mariner, Lunar Orbiter, Gemini, and Surveyor spacecraft
Vibration and acoustic environments for payload/cargo integration
Shuttle orbiter launch vibration and acoustic environments for cargo bay/payload interfaces are predicted. Data acquired during Shuttle flight tests are compared with the preflight estimates. Vibration response data for payload attachment locations are presented, along with acoustic data in the form of noise-level spectra measured at various locations in the cargo bay and space averages of the noise levels. It is shown that the payload-bay vibration and acoustic environments are generally less severe than predicted.
Mariner Mars 1964 acoustically induced vibration environment
Estimation of lift-off and transonic vibration spectra on Mariner Mars 1964 spacecraft to enhance survival probability in acoustically induced vibration environment during boost phase
Vibration and acoustic testing of spacecraft
Spacecraft are subjected to a variety of dynamics environments, which may include: quasi-static, vibration and acoustic loads at launch: pyrotechnic shocks generated by separation mechanisms; on orbit jitter; and sometimes, planetary landing loads. There is a trend in the aerospace industry to rely more on structural analyses and less on testing to simulate these environments, because dynamics testing of spacecraft is time consuming, risky and expensive.
Compilation of flight data from Titan III VEHICLES
Vibration, acoustic, and shock data for Titan III flight vehicle
Shuttle payload bay dynamic environments: Summary and conclusion report for STS flights 1-5 and 9
The vibration, acoustic and low frequency loads data from the first 5 shuttle flights are presented. The engineering analysis of that data is also presented. Vibroacoustic data from STS-9 are also presented because they represent the only data taken on a large payload. Payload dynamic environment predictions developed by the participation of various NASA and industrial centers are presented along with a comparison of analytical loads methodology predictions with flight data, including a brief description of the methodologies employed in developing those predictions for payloads. The review of prediction methodologies illustrates how different centers have approached the problems of developing shuttle dynamic environmental predictions and criteria. Ongoing research activities related to the shuttle dynamic environments are also described. Analytical software recently developed for the prediction of payload acoustic and vibration environments are also described.
Improved Bayesian regularization of inverse problems in vibrations and acoustics using noise-only measurements
Here, this paper studies Tikhonov regularization (ridge regression) parameter selection for problems in vibrations and acoustics. The selection method is based on a popular Bayesian method, but it incorporates measurements of sensor noise. The regularization parameter is closely related to the ratio of system input energy to noise energy, so noise measurements inform the inference procedure and improve parameter identification. In cases where standard Bayesian regularization identifies zero as the optimal regularization parameter, noise measurements guarantee a unique nonzero optimum. Sufficient theoretical criteria are developed for this guarantee. The method is verified in even-determined and under-determined configurations in an acoustic source localization simulation and a vibration load identification experiment. It is shown to yield significant improvements over existing empirical Bayesian regularization. Improvements are larger in the even-determined case and smaller in the under-determined case, wherein the inverse solution is less sensitive to the regularization parameter.
Coupling between plate vibration and acoustic radiation
A detailed numerical investigation of the coupling between the vibration of a flexible plate and the acoustic radiation is performed. The nonlinear Euler equations are used to describe the acoustic fluid while the nonlinear plate equation is used to describe the plate vibration. Linear, nonlinear, and quasi-periodic or chaotic vibrations and the resultant acoustic radiation are analyzed. We find that for the linear plate response, acoustic coupling is negligible. However, for the nonlinear and chaotic responses, acoustic coupling has a significant effect on the vibration level as the loading increases. The radiated pressure from a plate undergoing nonlinear or chaotic vibrations is found to propagate nonlinearly into the far-field. However, the nonlinearity due to wave propagation is much weaker than that due to the plate vibrations. As the acoustic wave propagates into the far-field, the relative difference in level between the fundamental and its harmonics and subharmonics decreases with distance.