There is also pro38.com, the manufacturer's website. On May 25, 2013 3:53 PM, "Mike Riss" <rockt_dude@xxxxxxxxxxxxx> wrote: > I'd like to second Jeff's referral to a great rocketry resource: > > thrustcurve.org > > You can look at the complete thrust curve over time, and in particular, > the initial thrust. Look in the "Simulator Section" under "Options", one > of which is "View Data" (the icon with the magnifying glass). The initial > graph is in newtons, but there's an option to display in pounds. > > Mike > > --- On *Sat, 5/25/13, Jeff Gortatowsky <indanapt@xxxxxxxxx>* wrote: > > > From: Jeff Gortatowsky <indanapt@xxxxxxxxx> > Subject: [roc-chat] Re: Clarification > To: "roc-chat@xxxxxxxxxxxxx" <roc-chat@xxxxxxxxxxxxx> > Date: Saturday, May 25, 2013, 12:22 PM > > Chris I have always used average thrust. But Carlo is right. The first > second of thrust appears to be about 45 or so pounds of thrust. That is a > guess from looking at the ROCKSIM graph on thrustcurve.org. > > I have a rocket at 6.5 pounds, and an I100 with a 5 ft guide reaches 41 > ft/sec at guide departure (according to RS). I consider anything above 35 > to ft/sec fine under normal conditions. (I have gone as low as 28 to 30 tho > some say that is too slow. But on a calm day I've done it.) > > --------------------------------------- > Jeff Gortatowsky, Redondo Beach, CA | Twitter: JeffGortatowsky | Yahoo: > indanapt > "(Scientific) Skepticism is not a set of beliefs, it is a set of methods > for asking questions about reality." -- Doctor Steven Novella > > ------------------------------ > *From:* Chris Coffee <chris_coffee@xxxxxxxxxx> > *To:* roc-chat@xxxxxxxxxxxxx > *Sent:* Friday, May 24, 2013 8:22 PM > *Subject:* [roc-chat] Clarification > > A little help here, please? I need to know if someone can tell me if my > calculations are correct for a Thrust-To-Weight calculation for an upcoming > flight...and whether or not the rocket should be flown on said motor? Thank > you. > > > Madcow Sensor weighing in at 7 pounds on the pad. 54mm motor mount. Using > a Cesaroni I100-RL-LB this is what I got: > > Average thrust of motor (according to ThrustCurve) = 98.5Ns > > Divide 98.5Ns by 4.45 to get 22.13 average thrust in pounds > > Divide 22.13 pounds of average thrust by 7 to get a Thrust-To-Weight ratio > of 3.16:1 > > Is this correct? > > If my math is correct, I would say that the rocket should not be flown > with the I100. > > Okay, folks.....school me!!! LOL > > > Christopher L. Coffee > > >