1 |
이규준, 소형분력시험대의 설계기법 연구, 국방과학연구소, MSDC-421-990614, 1999, 7/
|
|
2 |
ESDU 85032, "Ejectors and jet Pumps- Design and Performance for Incompressible Liquid flow", 1985/
|
|
3 |
MIL-HDBK-83728 "Criteria For Explosive Systems And Devices Used On Space Vehicles", 01 Jan. 1999, pp.22, 55-62/
|
|
4 |
T. Y. Chang and R. L. Thompson, "A Computer Program for Predicting Nonlinear Uniaxial Material Response Using Viscoplastic Models," NASA TM-83675, July 1984/
|
|
5 |
"Solid Rocket Motor Nozzles Space Vehicle Design Criteria(Chemical Propulsion)," NASA-SP-8115, June 1975/
|
|
6 |
Liquid Rocket Engine Combustion Stabilization Devices, NASA SP-8113, 1974/
|
|
7 |
Liquid Rocket Engine Injectors, NASA SP-8089, 1976/
|
|
8 |
NASA Space Vehicle Design Criteria, "Liquid Rocket Engine Fluid-Cooled Combustion Chambers," NASA Lewis Research Center, NASA SP-8087, April, 1972/
|
|
9 |
NASA, Solid Rocket Motor Igniters", NASA SP-8051, 1971, p.71 /
|
|
10 |
Research report, Solid Rocket motor performance analysis and prediction, NASA SP-8039, 1971/
|
|