Translatory shock absorber for attitude sensors
Abstract
A translatory shock absorber is provided for mounting an attitude sensor thereon for isolating a sensor from translatory vibrations. The translatory shock absorber includes a hollow block structure formed as one piece to form a parallelogram. The absorber block structure includes a movable top plate for supporting the attitude sensor and a fixed base plate with opposed side plates interposed between. At the junctions of the side plates, and the base and top plates, there are provided grooves which act as flexible hinges for attenuating translatory vibrations. A damping material is supported on a pedestal which is carried on the base plate between the side plates thereof. The top of the damping material rests against the bottom surface of the top plate for eliminating the resonant peaks of vibration.
- Publication:
-
NASA Marshall Space Flight Center Report
- Pub Date:
- April 1976
- Bibcode:
- 1976msfc.reptQ....V
- Keywords:
-
- Attitude Indicators;
- Mounting;
- Shock Absorbers;
- Patent Policy;
- Patents;
- Translational Motion;
- Vibration Damping;
- Spacecraft Instrumentation