| | [No title] (Site not responding. Last check: 2007-11-03) |
 | | It is anticipated that future turbine-based propulsion systems such as turbojet, turbo ramjet, and air turborocket will be capable of higher compressor pressure ratio and higher turbine temperature and will be capable of operating at higher Mach number. |
 | | By the year 2015 it is anticipated a turbine-based propulsion system could be operational that could provide the required specific impulse and thrust necessary to operate across a Mach number range from subsonic to about Mach 3 to 5. |
 | | Alternative Baseline Concepts and Subsystems Evaluation The alternative baseline concepts and their subsystems will be evaluated against the requirements of Section 2.0, using the Georgia Tech TMD methods or similar conceptual design and analysis tools. |
| www.asdl.gatech.edu /research_teams/images/Multi-MissionCruiseMissile1.doc (2676 words) |