It is important to realize that some test-articles may have significant sound absorption that may challenge the acoustic power capabilities of a test facility. Therefore, to mitigate this risk of not being able to meet the customers target spectrum, it is prudent to demonstrate early-on an increased acoustic power capability which compensates for this test-article absorption. This paper describes a concise method to reduce this risk when testing aerospace test-articles which have significant absorption. This method was successfully applied during the SpaceX Falcon 9 Payload Fairing acoustic test program at the NASA Glenn Research Center Plum Brook Stations RATF
Calculation methods for vibration responses of spacecraft structural members to acoustic field
Large reverberant chambers have been used for several decades in the aerospace industry to test larg...
A spacecraft at launch is subjected to a harsh acoustic and vibration environment resulting from the...
The exposure of a customer's aerospace test-article to a simulated acoustic launch environment is ty...
The exposure of a customers aerospace test-article to a simulated acoustic launch environment is typ...
The Structural Acoustics Loads and Transmission (SALT) facility at the NASA Langley Research Center ...
NASA Lewis Research Center recently led a multi-organizational acoustic test program. This testing c...
An initial acoustic calibration was performed for the NASA Langley Research Center reverberation cha...
The performance of a medium size, truncated reverberation chamber is evaluated in detail. Chamber pe...
The Acoustical Testing Laboratory (ATL) consists of a 27 by 23 by 20 ft (height) convertible hemi/an...
External acoustic environments, structural responses, noise reductions, and the internal acoustic en...
Analytical models have been developed to predict the sound absorption and sound transmission loss of...
NASA Lewis Research Center, in conjunction with General Dynamics Space Systems Division, has perform...
The NASA John H. Glenn Research Center at Lewis Field has designed and constructed an Acoustical Tes...
A recent operational need for the development of a large (101,000 ft 3) reverberant acoustic chamber...
Calculation methods for vibration responses of spacecraft structural members to acoustic field
Large reverberant chambers have been used for several decades in the aerospace industry to test larg...
A spacecraft at launch is subjected to a harsh acoustic and vibration environment resulting from the...
The exposure of a customer's aerospace test-article to a simulated acoustic launch environment is ty...
The exposure of a customers aerospace test-article to a simulated acoustic launch environment is typ...
The Structural Acoustics Loads and Transmission (SALT) facility at the NASA Langley Research Center ...
NASA Lewis Research Center recently led a multi-organizational acoustic test program. This testing c...
An initial acoustic calibration was performed for the NASA Langley Research Center reverberation cha...
The performance of a medium size, truncated reverberation chamber is evaluated in detail. Chamber pe...
The Acoustical Testing Laboratory (ATL) consists of a 27 by 23 by 20 ft (height) convertible hemi/an...
External acoustic environments, structural responses, noise reductions, and the internal acoustic en...
Analytical models have been developed to predict the sound absorption and sound transmission loss of...
NASA Lewis Research Center, in conjunction with General Dynamics Space Systems Division, has perform...
The NASA John H. Glenn Research Center at Lewis Field has designed and constructed an Acoustical Tes...
A recent operational need for the development of a large (101,000 ft 3) reverberant acoustic chamber...
Calculation methods for vibration responses of spacecraft structural members to acoustic field
Large reverberant chambers have been used for several decades in the aerospace industry to test larg...
A spacecraft at launch is subjected to a harsh acoustic and vibration environment resulting from the...