1 |
Hammond, W.E. Space Transportation : A Systems Approach to Analysis and Design, AIAA Education Series, Washington D.C., 1999.
|
2 |
Huang, Z., Fint, J.A., and Kuck, F.M., Key Reliability Drivers of Liquid Propulsion Engines and a Reliability Model for Sensitivity Analysis, In: The Boeing Company, Rocketdyne Propulsion & Power, 41st AIAA Joint Propulsion Conference & Exhibit, Vol. 10, 2005.
|
3 |
Seo, Y-K, and Oh, B-S, KSLV-II Cost Estimate using TRANSCOST 7.1, Aerospace Engineering and Technology, Vol. 6, No.2, 2007, pp.119-125.
|
4 |
Yoo, I-S, Seo, Y-K, Lee, J-H, and Oh, B-S, Application of Cost Estimation to Space Launch Vehicle Development Program, Journal of the Society of Korea Industrial and Systems Engineering, Vol.30, No.3, 2007, pp.165-173.
|
5 |
Koelle, D.E., Handbook of Cost Engineering for Space Transportation Systems with TRANSCOST 8.0, 2010, TransCostSystem.
|
6 |
Adams, J.D., Hickman, R.A., and Mayberry J.P., Payload Interface Standardization, 46th International Astronatuical Congress, October 2-6, Oslo, Norway, 1995.
|
7 |
Kececioglu, D. Reliability Engineering Handbook, Volume 2, 1991.
|
8 |
NASA, Exploration Systems Architecture Study, Final Report, Appendix 6D, 2005 November, pp. 194-195.
|
9 |
Kim, K.O. and Hwang, J.W., A Methodology for Estimating Reliability and Development Cost of a New Liquid Rocket Engine-focused on Staged Combustion Cycle with LOX/LH2, Journal of the Korean Society for Aeronautical & Space Sciences, Vol. 42, No. 2, 2014, pp. 437-443.
DOI
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