1 |
Ren, W. M., and Nally, J. F., "Computations of hollow-cone sprays from a pressure-swirl injector," SAE Paper 982610, 1998/
|
|
2 |
김중근 외 5명, "대형 연소시험대 교정 및 연소시험 분석 프로그램 개발 보고서, 국방과학연구소 보고서", MSDC-521-980906/
|
|
3 |
Xu, M., and Markle, L. E., "CFD-aided development of spray for an outwardly opening direct injection gasoline injector," SAE Paper 980493, 1998/
|
|
4 |
Rubin, S., "Instability Model of Missile Longitudinal Oscillation due to Propulsion Feedback," NASA, 68N86933, 1964/
|
|
5 |
Douglass, H. W., Collins Jr., J. H., Ellis, R. A. and Keller Jr., R. B., "Solid Rocket Motor Nozzles," NASA SP-8115, 1975/
|
|
6 |
Keller, R. B., Jr. (Ed.), Liquid Rocket Engine Combustion Stabilization Devices, NASA SP-8113, 1974/
|
|
7 |
Anon., "Pressurization Systems for Liquid Rockets," NASA Space Vehicle Design Criteria Monograph, SP-8112, October 1975/
|
|
8 |
NASA SP-8107, "Turbopump Systems for Liquid Rocket Engines," 1974, pp.86/
|
|
9 |
NASA SP 8097, "Liquid Rocket Valve Assemblies," 1973, pp.11/
|
|
10 |
Liquid rocket engine fluid-cooled combustion chamber, NASA SP-8087, 1972/
|
|