Comparative Performance Study of Strain Gauge Sensors for Ion Thrust Measurement
Author:
Affiliation:
1. Department of Instrumentation, Indian Institute of Science
2. Control Systems Group, ISRO Satellite Center
Publisher
Institute of Electrical Engineers of Japan (IEE Japan)
Subject
Electrical and Electronic Engineering,Mechanical Engineering
Link
http://www.jstage.jst.go.jp/article/ieejsmas/125/12/125_12_479/_pdf
Reference10 articles.
1. (1) K. Makowski, Z. Peradzynski, N. Gascon, and M. Dudeck: “A Stationary Model for Stationary Plasma Thruster (SPT) Discharge”, Proc. of 35th AIAA/ASME/SAE/SEE Joint Propulsion Conference & Exhibit, Los Angeles, California, USA, June 20-24, AIAA pp. 99-2295 (1999)
2. (2) L. Garrigues, A. Heron, J. C. Adam, and J. P. Boeuf: “Comparisons Between Hybrid & PIC Models of Stationary Plasma Thruster”, Proc. of 35th AIAA/ASME/SAE/ASEE, Joint Propulsion Conference & Exhibit, Los Angeles, California, USA, June 20-24, paper AIAA-99-2297 (1999)
3. (3) S. Roche, S. Barral, S. Bechu, M. Dudeck, P. Lasgorceix, L. Magne, T. Minea, D. Pagnon, and M. Touzeau: “Thermal Analysis of a Stationary Plasma Thruster”, Proc. of 35th AIAA/ASME/SAE/SEE, Joint Propulsion Conference & Exhibit, Los Angeles, California, USA, June 20-24, paper AIAA 99-2296.
4. (4) M. Day, N. Maslennikov, T. Randolph, and W. Rogers: “SPT-100 Subsystem Qualification Status”, Proc. of 31st AIAA/ASME/SAE/ASEE, Joint Propulsion Conference and Exhibit, San Diego, CA, USA, July 10-12, AIAA-95-2666 (1995)
5. Strain gauge based thrust measurement system for a stationary plasma thruster
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