Average thrust limit?

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smstachwick

LPR/MPR sport flier with an eye to HPR and scale
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I seem to recall reading in Stine’s Handbook of Model Rocketry that the average thrust of a model rocket motor (as opposed to a high-power rocket motor) is limited to 80 Newtons. Looking at sources from AeroTech however, it appears that there are several G motors available that exceed this and don’t have a requirement for an L1 certification, like the G104T, G125T, and G339N.

The only G motors ones I see that require it are the G75M, presumably for using the sparky Metalstorm propellant, and the G138T, for reasons I can’t seem to identify.

So what exactly are the criteria for classification as a model rocket motor vs a high-power one? It seems that some of the G motors available are classified arbitrarily.
 
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Looking at sources from AeroTech however, it appears that there are several G motors available that exceed this and don’t have a requirement for an L1 certification, like the G104T, G125T, and G339N.

An L1 is required to purchase these three. Check dealers such as csrocketry or apogee and you will see it is a requirement.
 
According to their website, an L1 is required to purchase these three.
Interesting. I should have dug a little deeper, Apogee says the same thing about the reload kits in their store.

Looks like some sloppy research on my part. Note to self: Check the Motor Matrix AND the other parts of the site before posing a question to the forum.
 
Thank you! That was my understanding of the MPR/HPR threshold, looks like I just came across some inaccurate data and failed to cross-check it.

Nice graphics, too. Where did you find this?
 
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