Torsional thrust stand for characterization of microthrusters

• Main Authors: Cheah, K.H, Low, K.S
• Other Authors: ELECTRICAL AND COMPUTER ENGINEERING
• Format: Conference or Workshop Item
• Published: 2020
• Subjects: Aerospace engineering; Calibration; Constant force; Impulse bit; Micro thruster; Steady state; Thrust stand; Torsional pendulum; Pulsed plasma thrusters
• Online Access: https://scholarbank.nus.edu.sg/handle/10635/179907
• Institution: National University of Singapore

10.1088/1757-899X/152/1/012019