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Systems integration studies for supersonic cruise aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mascitti, V. R. |
| Copyright Year | 1975 |
| Description | Technical progress in each of the disciplinary research areas affecting the design of supersonic cruise aircraft is discussed. The NASA AST/SCAR Program supported the integration of these technical advances into supersonic cruise aircraft configuration concepts. While the baseline concepts reflect differing design philosophy, all reflect a level of economic performance considerably above the current foreign aircraft as well as the former U.S. SST. Range-payload characteristics of the study configurating show significant improvement, while meeting environmental goals such as takeoff and landing noise and upper atmospheric pollution. |
| File Size | 1424878 |
| Page Count | 33 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760004953 |
| Archival Resource Key | ark:/13960/t6n05xc3s |
| Language | English |
| Publisher Date | 1975-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Hydrogen Fuels Noise Reduction Cost Reduction Aircraft Design Wing Profiles Supersonic Transports Aircraft Configurations Turbojet Engines 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 |