1 |
Lee, H. J., and Kang, E. S., "Development of Direct Drive Electro-mechanical Actuation System for Thrust Vector Control of KSLV-II," Journal of The Korean Society for Aeronautical and Space Science, Vol. 44, No. 10, 2016, pp.911-920.
DOI
|
2 |
Jeon, S. W., "A Study on the Limit Cycle Analysis of the Reaction Control System for Satellite Launch Vehicle," Chungnam National University, 2010.
|
3 |
Gotzig, U., "Challenges and Economic Benefits of Green Propellants for satellite Propulsion," 7th European conference for Aeronautics and Space Sciences(EUCASS2017- 639), 2017.
|
4 |
Cho, I. H., Han, S. Y., Yoon, H. S., and Lee, J. W., "Review of the Attitude Control for Space Launcher Vehicle," Proceeding of The Korean Society for Aeronautical and Space Sciences Fall Conference, November 2015, pp.1917-1920.
|
5 |
An, S. Y., "Design of Monopropellant Thruster with Consideration of Response Characteristics for Attitude Control System," Korea Advanced Institute of Science ann Technology, 2010.
|
6 |
Bombelli, V., Simon, D., and Maree, T., "Economic Benefits of The Use of Non-Toxic Mono-Propellants for Spacecraft Applications," AIAA 2003-4784.
|
7 |
Kajon, D., et al., "Development of an Attitude Control and Propellant Settling System for the aA5ME Upper Stage," Space Propulsion Conference. Cologne, Germany, May 19. 2014.
|
8 |
Amri, R., Gibbon, D., and Rezoug, T., "The Design, development and test of one newton hydrogen peroxide monopropellant thruster," Aerospace Science and Technology, Vol. 25, Issue 1, March 2013, pp.266-272.
DOI
|
9 |
Ventura, M., Wernimont, E., Heister, S., and Yuan, S., "Rocket Grade Hydrogen Peroxide(RGHP) for use in Propulsion and Power Devices-Historical Discussion of Hazards," In: The 43rd AIAA/ASME/SAE/ASEE joint propulsion conference& exhibit, Cincinnati, OH, USA, July 8-11 2007, AIAA 2007-5468.
|
10 |
Gordon, S., and MacBride, B. J., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications," NASA, Ref. Publ. 1311, October 1994.
|