Accession Number : ADA017854
Title : Development and Demonstration of a Cast Propellant for the LANCE Igniter Grain.
Descriptive Note : Technical rept.,
Corporate Author : ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL ALA PROPULSION DIRECTORATE
Personal Author(s) : Allen,Henry C. ; Cucksee,Marjorie T.
Report Date : 10 SEP 1975
Pagination or Media Count : 42
Abstract : A cast composite propellant based on a HTPB binder was developed to meet the ballistic and physical requirements of the LANCE igniter grain. Formulation parameters were correlated with propellant burn rate and mechanical properties, and 1-gallon mixes were made to provide grains for a feasibility demonstration. The propellant was scaled up to a 20-gallon mixer, and grains were prepared for a prequalification demonstration task. Propellant performance in the 26-shot demonstration firing series was completely successful. The propellant is considered to be ready for qualification in the LANCE igniter.
Descriptors : *Surface to surface missiles, *Solid rocket propellants, *Rocket igniters, Malfunctions, Rocket propellant grains, Casting, Burning rate, Solid rocket propellant binders, Safety and arming(Ordnance)
Subject Categories : Surface-launched Guided Missiles
Solid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE