Experimental vibration studies performed on a number of flight control moment gyros and bearing life test fixtures are summarized. Tests were performed at MSFC, at Wyle Laboratories, Huntsville, Alabama, and at the Bendix Corporation facilities in Teterboro, New Jersey. A description of test and analysis equipment is included as well as test procedures and overall performance rankings. Advanced ultrasonic rolling element bearing fault detection techniques were applied for bearing analysis along with conventional vibration and sound analysis procedures
The application of vibration, as the sensing medium for measurements in predictive and preventive ma...
Vibration testing spaceflight hardware is a vital, but time consuming and expensive endeavor. Tradit...
Ground vibration tests were conducted on a YF-12 airplane. To approximate a structural free-free bou...
In 2005, the University of South Carolina (USC) was given the unique opportunity of studying...
This report investigates half-sine shock and sinusoidal vibration tests of gas bearing supported rot...
NASA-HDBK-7008 Spacecraft Level Dynamic Environments Testing discusses the approaches, benefits, dan...
A bearing damper, operating on the support flexure of a pivoted pad in a tilting-pad type gas-lubric...
A complete ground vibration and aeroelastic analysis was made of a modified version of the Grumman A...
Bearings generate disturbances that, when combined with structural gains of a momentum wheel, contri...
This report presents test results of experiments on the vibration-response characteristics of airpla...
The design and development are presented of a gimballed gyro and breadboard equipment. Test results ...
A test program was conducted with the objective of developing a method and equipment for on-line mon...
A new method of conducting lab vibration tests of spacecraft equipment was developed to more closely...
An executive summary and an analysis of the results are discussed. A user's guide for the digital co...
Calculation methods for vibration responses of spacecraft structural members to acoustic field
The application of vibration, as the sensing medium for measurements in predictive and preventive ma...
Vibration testing spaceflight hardware is a vital, but time consuming and expensive endeavor. Tradit...
Ground vibration tests were conducted on a YF-12 airplane. To approximate a structural free-free bou...
In 2005, the University of South Carolina (USC) was given the unique opportunity of studying...
This report investigates half-sine shock and sinusoidal vibration tests of gas bearing supported rot...
NASA-HDBK-7008 Spacecraft Level Dynamic Environments Testing discusses the approaches, benefits, dan...
A bearing damper, operating on the support flexure of a pivoted pad in a tilting-pad type gas-lubric...
A complete ground vibration and aeroelastic analysis was made of a modified version of the Grumman A...
Bearings generate disturbances that, when combined with structural gains of a momentum wheel, contri...
This report presents test results of experiments on the vibration-response characteristics of airpla...
The design and development are presented of a gimballed gyro and breadboard equipment. Test results ...
A test program was conducted with the objective of developing a method and equipment for on-line mon...
A new method of conducting lab vibration tests of spacecraft equipment was developed to more closely...
An executive summary and an analysis of the results are discussed. A user's guide for the digital co...
Calculation methods for vibration responses of spacecraft structural members to acoustic field
The application of vibration, as the sensing medium for measurements in predictive and preventive ma...
Vibration testing spaceflight hardware is a vital, but time consuming and expensive endeavor. Tradit...
Ground vibration tests were conducted on a YF-12 airplane. To approximate a structural free-free bou...