A Characterized Status Report on Pulse Detonation Engine
Journal Title: INCAS BULLETIN - Year 2019, Vol 11, Issue 2
Abstract
Pulse Detonation Engine (PDE), is an exciting propulsion technology for the future and has been able to seek considerable attention over the last era. It has the potential to work efficiently in the modern cosmos. It works on a Humphrey cycle offering a great opportunity, which outweighs the conventional Brayton cycle. The operating cycle of PDE starts with the fuel-oxidizer mixture, combustion and DDT followed by purging. The PDE combustion process, which is a unique process, leads to consistent and repeatable detonation waves. This pulsed detonation combustion process causes rapid burning of the fuel-oxidizer mixture, which cannot be seen in any other combustion process as it is a thousand times faster than any other mode of combustion. PDE not only holds the capability of running effectively up to Mach 5 but it also changes the technicalities in space propulsion. The present study deals with the categorization of design approach, thermal analysis, performance analysis, fuel-based analysis, PDE combustors, detonation propagation, experimentation analysis, valving techniques, ignition studies, parameters & specification optimization, instrumentation, thrusters, parameters affecting specific impulse & thrust, hybrid PDE’s & turbine integration.
Authors and Affiliations
Bharat Ankur DOGRA, Mehakveer SINGH, T. K. JINDAL
Keywords
Related Articles
- EP ID EP585123
- DOI 10.13111/2066-8201.2019.11.2.6
- Views 81
- Downloads 0
Method of formalizing the layout of the internal compartments of aircraft
The mathematical formulation of the aircraft’s internal layout problem is described as an optimization problem, with an indication of its objective function, constraints, and performance criteria. The approach (receptor...
FOREWORD
Static and Dynamic Design Methods for Hybrid Bolted Joints in a Satellite Structure
A detailed analytical design for hybrid (metal-composite) bolted joints in static and dynamic (random vibrations) analysis is presented in this paper. Due to the fact that a space structure must be lighter and stiffened,...
Design and Analysis of Flapping Wing Micro Aerial Vehicle using Magnetic Levitation Technique
This research approaches the design and analysis of micro aerial vehicle with flapping wing mechanism by using magnetic levitation technique. Insects flight has created wide impacts in aerospace engineering due to its ae...
The Use of Satellite Technologies for Maritime Surveillance: An Overview of EU Initiatives
The sea lies at the heart of the EU prosperity and security: the Union and its member states depend on open and secure seas and oceans for their trade, transportation, energy, food, mineral resources, tourism, and a heal...