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The perfectly ideal accelerometer
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Stuhlinger, Ernst |
| Copyright Year | 1990 |
| Description | Given here is a condensed version of the results and conclusions that developed during the Workshop. Upper limits of residual accelerations that can be tolerated during materials processes, presented as acceptable and as desirable limits, are shown. Designs and capabilities of various accelerometers, and their inherent problems, are compared. Results of acceleration measurements on Spacelab flights are summarized, and expected acceleration levels on the Space Station under various conditions are estimated. |
| File Size | 598783 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910003114 |
| Archival Resource Key | ark:/13960/t0gv0h92z |
| Language | English |
| Publisher Date | 1990-08-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Instrumentation Accelerometers Crystal Growth Spacelab Drag Conferences Structural Vibration Estimating Space Processing Spacecraft Environments Design Analysis Space Stations Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
