Torsional thrust stand for characterization of microthrusters

Torsional thrust stand for characterization of microthrusters

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

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Bibliographic Details
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
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Institution: National University of Singapore

Internet

https://scholarbank.nus.edu.sg/handle/10635/179907

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