Development of a microprocessor-based instrument for static testing small rocket engines.

Distinguished Alumni Award Program author. Arthur H. Barber, III (Presented 25 February 2013) === A microprocessor-based instrument was developed for static testing solid-fuel rocket engines having peak thrusts of 130 Newtons or less and total impulses of up to 100 Newton-seconds.It measured peak t...

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Bibliographic Details
Main Author: Barber, Arthur Houghton
Other Authors: Cotton, M.L.
Language:en_US
Published: Monterey, California. Naval Postgraduate School 2012
Online Access:http://hdl.handle.net/10945/18681