Document Details

Determination of the Effective Rocket Propellant Transient Temperatures in Simulated Arctic Wintertime and Tropical Desert Summertime Climates
Ligocki, J E [Organization 1332]
Document Type:
Publication Date:
1955 Mar 10
Document Pages:
15 p.
Document Number(s):
SC-TM-035-55(13); ALSNL199700000772
Originating Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
OpenNet Entry Date:
1999 Sep 28
OpenNet Modified Date:
1999 Sep 28
This is a study of the effects of storage under varying environmental conditions on the effective solid propellant grain temperature. The range of a rocket-propelled missile is sensitive to variations in the effected burn time of the rocket motor.

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