التفاصيل البيبلوغرافية
| العنوان: |
Iodine Hall-Effect Electric Propulsion System Research, Development, and System Durability Demonstration |
| المؤلفون: |
Haag, Thomas W., Kamhawi, Hani, Costa, Gustavo C. C., Benavides, Gabriel F., Mackey, Jonathan A. |
| المصدر: |
CASI |
| سنة النشر: |
2018 |
| المجموعة: |
NASA Technical Reports Server (NTRS) |
| مصطلحات موضوعية: |
Spacecraft Propulsion and Power |
| جغرافية الموضوع: |
Unclassified, Unlimited, Publicly available |
| الوصف: |
This paper reviews recent iodine electric propulsion research and development activities at the NASA Glenn Research Center (GRC). Activities included (i) investigation of the iodine compatibility of BaO-CaO-Al2O3 impregnated tungsten hollow cathodes based on a flight heritage design, (ii) investigation of the iodine compatibility of a handful of materials common to propulsion systems, spacecraft, and ground test facilities, (iii) development of reliable iodine feed system technologies, (iv) implementation of test facility improvements in an attempt to mitigate iodine associated negative impacts, and culminated in (v) an 1,174-hour hybrid iodine-xenon propulsion system durability demonstration (iodine fed Hall-effect thruster with xenon fed cathode). Each of the activities resulted in extensive insights that shall inform future iodine electric propulsion developments. While reliable operation of a BaO-CaO-Al2O3 impregnated tungsten hollow cathode on iodine vapor was not achieved, long-term operation on xenon gas in proximity to an iodine fed thruster was demonstrated without any measurable degradation or cross-contamination of the cathode. Furthermore, iodine material corrosion investigations conducted at 300degC over 5, 15, and 30 days showed significant deterioration of all materials evaluated, although the same materials with a silicon coating proved nearly impervious to iodine so long as the coating was not mechanically damaged. Finally, the 1,174-hour durability test demonstration showed that (i) iodine feed system technologies developed at GRC delivered well-regulated uninterrupted propellant, (ii) implementation of appropriate facility improvements and procedures can limit negative impacts of iodine on test hardware and ground support equipment, although facility challenges with iodine are extensive, and (iii) a Hall-effect thruster operates with similar performance whether employing iodine or xenon propellant over long durations. The work was motivated by strong government and commercial interest in the ... |
| نوع الوثيقة: |
other/unknown material |
| وصف الملف: |
application/pdf |
| اللغة: |
unknown |
| Relation: |
Document ID: 20180005337; http://hdl.handle.net/2060/20180005337 |
| الاتاحة: |
http://hdl.handle.net/2060/20180005337 |
| Rights: |
Copyright, Public use permitted |
| رقم الانضمام: |
edsbas.E915D618 |
| قاعدة البيانات: |
BASE |