The purpose of this Handbook is to provide guidance for dynamic environments testing of flight spacecraft, large instruments, associated dynamic test models (DTMs), and flight structure subsystems for the mission dynamics environments and loads. The emphasis of this Handbook is on vibration, acoustic, and shock environmental testing. Static and modal testing are discussed only in regard to the role each plays in complementing the dynamic testing in a complete structural qualification program. This Handbook concentrates on new dynamics testing methodologies but summarizes and provides key references for older dynamic test methodologies. NASA Endorsed. OCE.
| Edition : | Baseline |
| File Size : | 1
file
, 3.8 MB |
| Number of Pages : | 134 |
| Published : | 06/12/2014 |
