For Aerotech single use motors, try using first fire jr instead of the copperheads igniters.
For Estes or Quest motors, try the Quest q2g2 model rocket igniters.
http://www.thrustcurve.org/guidepage.jsp
Take motor average thrust in Newtons and divide by 4.45 to convert to pounds.
NAR requires a 3 to 1 safety margin but 5 to 1 is recommended.
For example, the dry weight of a rocket was 4 lbs and using a Cesaroni H152, which fully configured, was just under 1 lb for a launch weight of 5 lbs. It's average thrust was 152n, so 152/4.45/5=6.8lb. So there was a couple pounds to spare.
http://openrocket.sourceforge.net/index.html
http://www.tripolisandiego.org/
http://www.apogeerockets.com/e-zine_newsletter.asp#latest_newsletter_anchor
Thanks to Mr. Larry Hermanson for contributing content for this page.
Credit to "Modern High-Power Rocketry 2" by Mark Canepa for engine sizing calculations.