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Concept development of a mach 3.0 high-speed civil transport
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Martin, Glenn L. Morris Jr., Shelby J. Beissner Jr., Fred L. Swanson, E. E. Shields, E. W. Coen, Peter G. Robins, A. Warner Geiselhart, Karl Dollyhigh, Samuel M. |
| Copyright Year | 1988 |
| Description | A baseline concept for a Mach 3.0 high-speed civil transport concept was developed as part of a national program with the goal that concepts and technologies be developed which will enable an effective long-range high-speed civil transport system. The Mach 3.0 concept reported represents an aggressive application of advanced technology to achieve the design goals. The level of technology is generally considered to be that which could have a demonstrated availability date of 1995 to 2000. The results indicate that aircraft are technically feasible that could carry 250 passengers at Mach 3.0 cruise for a 6500 nautical mile range at a size, weight and performance level that allows it to fit into the existing world airport structure. The details of the configuration development, aerodynamic design, propulsion system design and integration, mass properties, mission performance, and sizing are presented. |
| File Size | 2244344 |
| Page Count | 54 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880017798 |
| Archival Resource Key | ark:/13960/t14n42x7p |
| Language | English |
| Publisher Date | 1988-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Aerodynamic Configurations Transport Aircraft Supersonic Cruise Aircraft Research Engine Airframe Integration Aircraft Performance Aircraft Design Supersonic Transports Sizing Aircraft Configurations Propulsion System Configurations Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |