• Created by Unknown User (astrocrg@mit.edu), last modified by Unknown User (reilleya@mit.edu) on Dec 12, 2017 14:42

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Overview

Due to materially inefficient casting procedures, the team had an excess of thermal liners for 98mm motors. This lead to the idea to attempt a monolithic grain casting directly in the thermal liner.

Manufacturing

The motor is designed to utilize a 98mm thermal liner from RCS, a hot-wired foam core, 3D printed end caps, and 12.5 lbs of propellant. This load should be compatible with any appropriate case.

Simulations

Sam A designed a Burnsim file for the motor, uploaded here.

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