@article{(Open Science Index):https://publications.waset.org/pdf/10611,
	  title     = {Development of a Thrust Measurement System},
	  author    = {S. Jeon and  J. Kim and  H. Choi},
	  country	= {},
	  institution	= {},
	  abstract     = {KSLV-I(Korea Space Launch Vehicle-I) is designed as
a launch vehicle to enter a 100 kg-class satellite to the LEO(Low Earth
Orbit). Attitude angles of the upper-stage, including roll, pitch and
yaw are controlled by the cold gas thruster system using nitrogen gas.
The cold gas thruster is an actuator in the RCS(Reaction Control
System). To design an attitude controller for the upper-stage, thrust
measurement in vacuum condition is required. In this paper, the new
thrust measurement system and calibration mechanism are developed
and measurement errors and signal processing method are presented.},
	    journal   = {International Journal of Aerospace and Mechanical Engineering},
	  volume    = {6},
	  number    = {3},
	  year      = {2012},
	  pages     = {645 - 649},
	  ee        = {https://publications.waset.org/pdf/10611},
	  url   	= {https://publications.waset.org/vol/63},
	  bibsource = {https://publications.waset.org/},
	  issn  	= {eISSN: 1307-6892},
	  publisher = {World Academy of Science, Engineering and Technology},
	  index 	= {Open Science Index 63, 2012},
	}