This paper is based on a prior paper by the same author entitled “Fragility Rating For Aircraft Equipment”. The analogy between accelerations caused by vibration and shock is discussed. Testing to establish a fragility rating is discussed and a rating is established for a Klystron based upon tests discussed in a companion paper. Comparative fragility data is presented, showing a wide scope of fragility, size, weight and loading.
FRAGILITY RATING: (AID TO PACKAGE DESIGN)
Sae Technical Papers
Pre-1964 SAE Technical Papers ; 1906
01.01.1955
Aufsatz (Konferenz)
Englisch
Engineering Index Backfile | 1955
|FRAGILITY RATING FOR AIRCRAFT EQUIPMENT: (POTENTIAL AID TO PACKAGE CUSHION DESIGN)
SAE Technical Papers | 1954
|Cushion design from fragility rating
Engineering Index Backfile | 1955
|Cushion Design From Fragility Rating
SAE Technical Papers | 1956
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