RAP opportunity at Naval Research Laboratory NRL
Plasma Infused Architected Thermionic Emitting Cathode Research
Location
Naval Research Laboratory, DC, Spacecraft Engineering Department
opportunity |
location |
|
64.15.86.C0649 |
Washington, DC 203755321 |
Advisers
name |
email |
phone |
|
Michael S McDonald |
michael.s.mcdonald80.civ@us.navy.mil |
202.404.3680 |
Description
The U.S. Naval Research Laboratory (NRL) Spacecraft Propulsion Section, part of the Spacecraft Engineering Division, maintains active research in reactive plasma sources with in close cooperation with the NRL Plasma Physics Division. The development of such plasma sources finds broad applications in both aerospace and plasma engineering, from plasma actuation to materials processing. In the area of plasma propulsion, the NRL Spacecraft Propulsion Section is developing novel high current electron sources using architected materials.
We seek excellent candidates to support research and development of these new electron sources for propulsion systems. This includes the measurement of plasma properties using in-situ and optical diagnostics to understand the principles of system efficiency and translate these fundamental findings into novel designs. The candidate will make use of modern manufacturing techniques for rapid prototyping and investigate the use of new materials to achieve the program goals. A highly qualified candidate will have demonstrated experience working with electric propulsion systems, in thermionic emission in plasmas, global modeling of plasmas, with standard plasma diagnostics such as Langmuir probes, and CAD. Ideally, the candidate will also has exposure or hands-on experience with and thermionic cathodes and Hall thrusters.
Candidates will interface with personnel in both the Spacecraft Engineering and Plasma Physics Divisions. Facilities available include high-vacuum test chambers and supporting equipment for plasma operation and plasma diagnostic evaluation in representative aerospace environments, dedicated ultra-high vacuum material characterization facilities, a wide variety of plasma diagnostic tools, high-power laser equipment, and access to DoD HPC simulation resources.
key words
Plasma; Cathode; Space; Spacecraft; Thermionic; Propulsion; Diagnostics; Experimental; Design; Test; Vacuum; Electron; Hall Thruster;
Eligibility
Citizenship:
Open to U.S. citizens and permanent residents
Level:
Open to Postdoctoral applicants
Stipend
Base Stipend |
Travel Allotment |
Supplementation |
|
$99,200.00 |
$3,000.00 |
|
|