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Titanium Optics for Ion Thrusters

Titanium Optics for Ion Thrusters PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 22

Book Description


Titanium Optics for Ion Thrusters

Titanium Optics for Ion Thrusters PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 22

Book Description


Performance of Titanium Optics on a NASA 30 Cm Ion Thruster

Performance of Titanium Optics on a NASA 30 Cm Ion Thruster PDF Author: George C. Soulas
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

Book Description


Titanium Optics for Ion Thrusters

Titanium Optics for Ion Thrusters PDF Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781724041883
Category : Science
Languages : en
Pages : 36

Book Description
Ion thruster total impulse capability is limited, in part, by accelerator grid sputter erosion. A development effort was initiated to identify a material with a lower accelerator grid volumetric sputter erosion rate than molybdenum, but that could utilize the present NSTAR thruster grid design and fabrication techniques to keep development costs low, and perform as well as molybdenum optics. After comparing the sputter erosion rates of several atomic materials to that of molybdenum at accelerator voltages, titanium was found to offer a 45% reduction in volumetric erosion rates. To ensure that screen grid sputter erosion rates are not higher at discharge chamber potentials, titanium and molybdenum sputter erosion rates were measured at these potentials. Preliminary results showed only a slightly higher volumetric erosion rate for titanium, so that screen grid erosion is insignificant. A number of material, thermal, and mechanical properties were also examined to identify any fabrication, launch environment, and thruster operation issues. Several titanium grid sets were successfully fabricated. A titanium grid set was mounted onto an NSTAR 30 cm engineering model ion thruster and tested to determine optics performance. The titanium optics operated successfully over the entire NSTAR power range of 0.5 to 2.3 kW. Differences in impingement-limited perveances and electron backstreaming limits were found to be due to a larger cold gap for the titanium optics. Discharge losses for titanium grids were lower than those for molybdenum, likely due to a slightly larger titanium screen grid open area fraction. Radial distributions of beam current density with titanium optics were very similar to those with molybdenum optics at all power levels. Temporal electron backstreaming limit measurements showed that titanium optics achieved thermal equilibrium faster than molybdenum optics. Soulas, George C. and Haag, Thomas W. and Patterson, Michael J. and Rawlin, Vincent K. Glenn Resear

Translation Optics for 30 Cm Ion Engine Thrust Vector Control

Translation Optics for 30 Cm Ion Engine Thrust Vector Control PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

Book Description


Performance Evaluation of 40 Cm Ion Optics for the NEXT Ion Engine

Performance Evaluation of 40 Cm Ion Optics for the NEXT Ion Engine PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 19

Book Description


Ion Engine and Hall Thruster Development at the NASA Glenn Research Center

Ion Engine and Hall Thruster Development at the NASA Glenn Research Center PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 18

Book Description


36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 2000-3800 - 2000-3849

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 2000-3800 - 2000-3849 PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 574

Book Description


A Multiple-cathode, High-power, Rectangular Ion Thruster Discharge Chamber for Increasing Thruster Lifetime

A Multiple-cathode, High-power, Rectangular Ion Thruster Discharge Chamber for Increasing Thruster Lifetime PDF Author: Joshua Lucas Rovey
Publisher:
ISBN:
Category :
Languages : en
Pages : 724

Book Description


38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 02-3800 - 02-3849

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 02-3800 - 02-3849 PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 394

Book Description


Microwave ECR Ion Thruster Development Activities at NASA Glenn Research Center

Microwave ECR Ion Thruster Development Activities at NASA Glenn Research Center PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 18

Book Description