Micro Pulse Detonation Rocket Engine for Nano-Satellite Propulsion

Completed TRL 3 (started at 1, targeting 3)

Description

The objective is to develop an efficient propulsion system that uses micro pulse detonation rocket engine (-PDRE) for nano-satellite maneuverability in space. The -PDRE is expected to provide a higher specific impulse and better volumetric efficiency in comparison with the currently available micro-thrusters. The -PDRE thrust could be easily controlled by changing the number of detonation pulses.

Details

Technology area	Propulsion Systems > Aero Propulsion > Airbreathing Pressure Gain Combustion
Program	Center Innovation Fund: GSFC CIF (GSFC CIF)
Lead organization	Goddard Space Flight Center, Greenbelt, MD
Start date	2011-10-01
End date	2012-09-01

Project contacts

Listed on TechPort itself — the most direct way to ask about this specific project.

Daniel J Ramspacher — daniel.j.ramspacher@nasa.gov

How to get involved

This is early/mid-stage (TRL 3) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

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