Verification criteria for small spaceflight components
Abstract
A philosophy is developed for vibration testing small components rocket and space-laboratory payloads. The structural requirements for Spacelab experiments are studied with the aim of clarifying the individual test objectives, placing more emphasis on the achievement of these objectives, rather than to such problems as ensuring a specific sweep rate or a dynamic input.
- Publication:
-
Deutsche Gesellschaft fuer Luft- und Raumfahrt and American Astronautical Society
- Pub Date:
- May 1980
- Bibcode:
- 1980dglr.meetT....M
- Keywords:
-
- Component Reliability;
- Reliability Analysis;
- Spacecraft Components;
- Vibration Tests;
- Dynamic Tests;
- Random Vibration;
- Spacelab Payloads;
- Vibration Mode;
- Spacecraft Instrumentation