Total Impulse Measuring System for Solid Propellant Rocket Engine: Phase I Report
ROCKETDYNE CANOGA PARK CA
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Discussion and results of three main considerations are presented 1 study and discussion of the use site and existing measurement system at EAFB, with recommendations for the installation of the Rocketdyne system 2 general and applied mathematical analyses of springmass total impulse measurement systems and 3 mechanical and electrical design of the Rocketdyne system to be constructed. Specific results of these separate but related program efforts are, respectively 1 concurrence with the general approach taken in the existing EAFB system, but disagreement with some specific design, installation, and operational features of the system 2 new and original mathematical analyses whose results justify the Rocketdyne approach to the measurement problem and 3 new and original mechanical and electrical component designs.
- Solid Propellant Rocket Engines