Combining the quasi-static loads, workmanship verification, and model validation tests of aerospace hardware into a single vibration test sequence can considerably reduce schedule and cost. The enabling factor in the implementation of the combined dynamic testing approach is the measurement of the dynamic forces exerted on the test item by the shaker. The dynamic testing of the QuikSCAT spacecraft is discussed as an example of a successful combined loads, workmanship, and model validation test program.
Combined Loads, Vibration, and Modal Testing of the QuikSCAT Spacecraft
Sae Technical Papers
World Aviation Congress & Exposition ; 1999
1999-10-19
Aufsatz (Konferenz)
Englisch
Combined Loads, Vibration, and Modal Testing of the QuikSCAT Spacecraft
British Library Conference Proceedings | 1999
|Combined Loads, Vibration, and Modal Testing of the QuikSCAT Spacecraft
British Library Conference Proceedings | 1999
|