Subhash Chander, Dr. TK Jindal
The aim of the paper is bring out integration challenges faced during “The design of a Pulse Tube for detonation of gaseous fuel using Acetylene and Oxygen. The detonation parameters are being analysed. The data generated will help in designing of pulse detonation propulsion system”. Due to these challenges, the performance of the system was significantly degraded and remedies became absolutely necessary. Paper also deals at length to deal the challenges faced including remedial actions in subsequent paras. Subsequently, the system results brought out are significantly encouraging.