1. The document describes the Promethean Igniter project which aims to develop an igniter for rocket engines with a burn time over 5 seconds and a chamber pressure of 521 psi. 2. It lists design assumptions including using frozen equilibrium calculations and measuring chamber pressure via a pressure transducer. Materials chosen are stainless steel 303 for machinability. 3. Objectives are outlined for a proof of concept including modifying the igniter for use with LOX/IPA propellants and measuring performance parameters.