{"id":1930,"date":"2010-01-30T15:06:26","date_gmt":"2010-01-30T23:06:26","guid":{"rendered":"http:\/\/rocketsnw.com\/?page_id=1930"},"modified":"2010-01-30T15:06:26","modified_gmt":"2010-01-30T23:06:26","slug":"bulk-plate-strength","status":"publish","type":"page","link":"https:\/\/northwestrocketry.com\/?page_id=1930","title":{"rendered":"Bulk plate strength"},"content":{"rendered":"<p>Article: 1930<br \/>\nBy Robert Krausert, January 2010<\/p>\n<p><strong>Carl Hamilton asked:<\/strong><br \/>\nIs there some easy way (i.e. for a non-materials engineer) to determine, roughly, how strong a bulk plate is going to be given a material, thickness, and diameter? Is there an easy way to determine how that strength will be effected by various holes drilled through the bulk plate? By strong, I mean, &#8220;How much force can be applied to the bulk plate through an attached U-bolt before it fails?&#8221; Is that shear strength?<\/p>\n<p><strong>Ray Stoner commented:<\/strong><br \/>\nYour bulk plate will generally be weaker than the glue joint in the body tube. I don&#8217;t believe I&#8217;ve ever seen a bulk plate fail in a &#8220;normal deployment&#8221;, nor have I seen many fail in a high speed deployment. It&#8217;s usually the recovery harness, or the &#8216;chute. Virtually all of the failures I&#8217;ve seen are in the glue joint between the bulk plate and the body tube.<\/p>\n<p>Figuring out the actual strength of the bulk plate is beyond me and I&#8217;ll leave it to others. The most science I&#8217;ve applied to it, is &#8220;this looks good enough&#8221;. The glue joint is where I&#8217;d focus my efforts.<\/p>\n<p>I&#8217;ve used as little as a 1\/4&#8243; thick Baltic Birch bulk plate in a 4&#8243; ~20 lbs bird without failure.<\/p>\n<p><strong>Ray Stoner commented:<\/strong><br \/>\nThe bulk plate will usually be STRONGER then the glue joint.<\/p>\n<p><strong>Steve Cutonilli commented:<\/strong><br \/>\nIt all comes down to chasing the weak sister in your system. I like Ray&#8217;s description of the glue joint going first &#8211; well, yeah except some of us always use a sliver of coupling tube on the load side of the bulkplate to increase the glue&#8217;s shear resistance and then one wonders why the eye-bolt yielded next.<\/p>\n<p>I will bet anyone on this list that the best measure to mitigate stresses to hard-points on your airframe is to use moderate length shock-cord (like we&#8217;ve heard of already) AND z-fold shock cord segments then wrap them with tape (figure a dozen segments typical on apogee cordage) &#8211; upon deployment the energy absorbed is significant.<\/p>\n<p>Or, attach a separate chute to each airframe segment and don&#8217;t worry about it (applies primarily to big massive rockets where hard-point stresses really factors more than normal).<\/p>\n<p><strong>Ken McGoffin commented:<\/strong><br \/>\nMy favorite. I use this even on a lot of model rockets. The whole idea is to absorb the kinetic energy of separation after the halves have separated a ways. The idea is NOT to bring the halves to a sudden, jerked halt with a short length of unyielding Kevlar or to bounce them back together with rubber bands or bungee cords.<\/p>\n<p>And this can also reduce the tangle of shock cord in the rocket.<\/p>\n<p><strong>John Armitage commented:<\/strong><br \/>\nI also like using the blue painter&#8217;s tape. I&#8217;ve actually had recoveries where all of the tape had not torn thru.<\/p>\n<p>The staggered shock absorbing is similar to, for those of you also in construction, a shock absorbing fall arrest lanyard for a body harness. The Flat nylon is Z-folded then stitched so that the stitches tear thru as the load is arrested.<\/p>\n<p>Also makes loading easier. I&#8217;ll bundle all the shock cords ahead of time, keeps &#8217;em nice and neat.<\/p>\n<p><strong>Bob Yanecek commented:<\/strong><br \/>\nKeith Stormo uses this &#8216;stitch&#8217; technique with great results. Key to the theory is to start (last z-fold to release) with multiple stitches, then ramp down the # of stitches as you continue with the Z-folding.<\/p>\n<p>This allows minimal force to begin unfolding but ever increasing force as the unfolding continues.<\/p>\n<p>If all z-folds pull loose, then next time around start with extra stitching with a goal of having that last one or two z-folds intact after fully deployed.<\/p>\n<p>This allows you to &#8216;measure&#8217; just how much force was exerted during deployment.<\/p>\n<p>With this technique, you can quite accurately determine force\/stitch required to pull it loose.<\/p>\n<p>I do something similar with blue tape and Kevlar but this does not allow much control over the force required to pull any particular z-fold loose. I do try and tape the begeesies out of the first z-folds and always look to see if they pull loose or not.<\/p>\n<p>My rational is that I&#8217;m using 1\/8&#8243; braided Kevlar and it&#8217;s kind of tough to stitch accurately (and still get 20&#8217;+ in 2&#8243; of 38mm airframe).<\/p>\n<p>Greatest risk is if your harness is too short. Either the shock of hitting the end locates a weak link or the recoil allows the parts to crash back together with a myriad of results. I recovered once with the weirdest hole in my upper airframe before (thanks again Keith!), determining the hole matched the eyebolt in my fin can.<\/p>\n<p><strong>Ken McGoffin commented:<\/strong><br \/>\nI like to see one or two bundles remaining at recovery. More, I&#8217;m wasting shock cord length. No remaining bundles, I figure a bit more energy should have been absorbed to keep stresses from shock down.<\/p>\n<p>But I can fly the same rocket on the same motor under the same conditions and end up with differing numbers of unopened bundles. It&#8217;s not an exact science but it is good practice IMO.<\/p>\n<p><strong>Ken McGoffin commented:<\/strong><br \/>\nYeah in my posts about this I was talking about taped Z-folds, small to mid-size rockets. Not terribly precise. Using it in a large and very expensive rocket stitching would be much better.<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Article: 1930 By Robert Krausert, January 2010 Carl Hamilton asked: Is there some easy way (i.e. for a non-materials engineer) to determine, roughly, how strong a bulk plate is going to be given a material, thickness, and diameter? Is there an easy way to determine how that strength will be effected by various holes drilled [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"parent":1903,"menu_order":0,"comment_status":"open","ping_status":"open","template":"","meta":{"ngg_post_thumbnail":0},"_links":{"self":[{"href":"https:\/\/northwestrocketry.com\/index.php?rest_route=\/wp\/v2\/pages\/1930"}],"collection":[{"href":"https:\/\/northwestrocketry.com\/index.php?rest_route=\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/northwestrocketry.com\/index.php?rest_route=\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/northwestrocketry.com\/index.php?rest_route=\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/northwestrocketry.com\/index.php?rest_route=%2Fwp%2Fv2%2Fcomments&post=1930"}],"version-history":[{"count":1,"href":"https:\/\/northwestrocketry.com\/index.php?rest_route=\/wp\/v2\/pages\/1930\/revisions"}],"predecessor-version":[{"id":1931,"href":"https:\/\/northwestrocketry.com\/index.php?rest_route=\/wp\/v2\/pages\/1930\/revisions\/1931"}],"up":[{"embeddable":true,"href":"https:\/\/northwestrocketry.com\/index.php?rest_route=\/wp\/v2\/pages\/1903"}],"wp:attachment":[{"href":"https:\/\/northwestrocketry.com\/index.php?rest_route=%2Fwp%2Fv2%2Fmedia&parent=1930"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}