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1
- #1
oreillsi
Aerospace
- Nov 6, 2012
- 11
Hi all,
On a project I'm working on I've been instructed that our first approach to determining the MoS values on the fasteners in a design wasn't correct and told to use the ECSS document on threaded fasteners (ECSS-E-HB-32-23A). I'm trying to implement the method in a spreadsheet now but it's just not really "clicking" with me somehow, has anyone got any experience in using this handbook for fastener/ joint design and analysis? The document can be downloaded from this link here:
Some (not many) of the chapters in the document have sample calculations in them which really helps to demonstrate the method but for the rest it just doesn't seem too clear, does anyone know perhaps where i might be able to read some previous examples of this method being used? Maybe a report of a previous design of a spacecraft/spacecraft's payload which used this standard for its joint analysis??
Any help would be greatly appreciated
On a project I'm working on I've been instructed that our first approach to determining the MoS values on the fasteners in a design wasn't correct and told to use the ECSS document on threaded fasteners (ECSS-E-HB-32-23A). I'm trying to implement the method in a spreadsheet now but it's just not really "clicking" with me somehow, has anyone got any experience in using this handbook for fastener/ joint design and analysis? The document can be downloaded from this link here:
Some (not many) of the chapters in the document have sample calculations in them which really helps to demonstrate the method but for the rest it just doesn't seem too clear, does anyone know perhaps where i might be able to read some previous examples of this method being used? Maybe a report of a previous design of a spacecraft/spacecraft's payload which used this standard for its joint analysis??
Any help would be greatly appreciated