Document Details
Title:
Static Test of 9641-31250 Intermediate Assembly
Author(s):
Grace, C M [North American Aviation, Inc. at Los Angeles International Airport]; Gaines, J W [North American Aviation, Inc.]; Schleicher, R L [North American Aviation, Inc.]
Document Type:
REPORT
Publication Date:
1954 Feb 01
Document Pages:
27 p.
Document Number(s):
SC-2594(TR); ALSNL199700000648
Originating Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
OpenNet Entry Date:
1999 Sep 28
OpenNet Modified Date:
1999 Sep 28
Description/Abstract:
All loads were applied by means of straps in conjunction with hydraulic struts. An Edison hydraulic pressure control unit was used to control loads on the specimen. For the ejection and chock load tests, five equally spaced cradles lined were used.