NASA/SP-8102, Space vehicle accelerometer applications, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance), NASA (Washington, DC, United States), December,1972, pp. 87, Format(s): PDF 4904k |
The physics of accelerometer applications are reviewed, and details are given on accelerometer instruments and the principles of their operations. The functions to which accelerometers are applied are listed, and terms commonly used in accelerometer reports are defined. Criteria guides state what rule, limitation, or standard must be imposed on each essential design element to insure successful design. Elaboration of these criteria in the form of recommended practices show how to satisfy each of these criteria, with the best procedure described when possible.
| Keywords: | space vehicles, accelerometers, spacecraft components, systems engineering, criteria, design, performance tests |
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| CASI Document ID Number: | 73N26891 |
| Subjects: | Astronautics: Spacecraft Instrumentation And Astrionics: Spacecraft And Aircraft Instrumentation |
| ID Code: | 131 |
| Deposited On: | 23 May 2002 |