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Micro Thruster Development with Green Propellant at mN and microN levels
Completed
TRL 3 (started at 1, targeting 3)
Description
The objective is to develop a high-efficiency micro-thruster using green propellant with electrospray injector that will ultimately provide micro-satellites with the performance required to enable the replacement of large, expensive, multi-role satellites with inexpensive, short-lead time, distributed systems of micro-satellites. The objectives of the project is the development of single emitter and multiple emitter injectors for doped kerosene; to develop a fundamental understanding of droplet transport, evaporation, and mixing in the complex swirling flow fields required for meso-scale flame stabilization; and the system integration of meso-scale thrust chamber with electrospray fuel injection system. A single emitter electrospray configuration will be developed and the performance benchmarked using Phase Doppler Particle Analysis to determine the droplet size distribution as a function of flow rate. The nature of droplet transport and evaporation at the meso-scale will be studied using non-intrusive laser based techniques. The electrospray injector will be integrated into the existing heat regenerating thrust chamber and fired with kerosene/H2O2.
Benefits
The development of these micro-thrusters would serve as a technology demonstration for a volumetrically efficient 3-axis stabilization and primary propulsion scheme for micro-satellite missions, providing the required high pointing accuracy and full range of attitude adjustment characteristic of larger satellites.
Details
| 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
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