1 |
Smith, C., Tomlinson, S., Gahn, S., Kretzing, J., Williams, R. and Hulett, W., "The Revolutionary Approach To Time-Critical Long Range Strike (RATTLRS) Propulsion System: Design Challenges and Lessons Learned," AIAA Missile Sciences Conference, AIAA-14-3, 16 November 2006
|
2 |
Mattingly, J. D., Heiser, W. H., Daley, D. H., Aircraft engine design, AIAA, 1987
|
3 |
EARLY, M., "Small Engine Component Technology(SECT) Program Final Report Technical Volume," NASA CR-175078, 1986
|
4 |
Kurzke, J., "The Mission Defines the Cycle: Turbojet, Turbofan and Variable Cycle Engines for High Speed Propulsion," NATO Science and Technology Organization, RTO-EN-AVT-185, 2010
|
5 |
Kurzke, J., GasTurb 10(Software) Manual, 2004
|
6 |
Kretzing, J. R., Snyder, C. D., "Evaluation of High-Mach Turbine Engines for Missile Applications," 26th JANNAF Airbreathing Propulsion Subcommittee Meeting, 01 April 2002, pp.43-55
|
7 |
Benstein, E., "An Assessment of Supersonic Gas Turbine Missile Propulsion Potential", AIAA 89-2471, 1989
|