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Closing the design loop on himat (highly maneuverable aircraft technology)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Robinson, M. R. Putnam, T. W. |
| Copyright Year | 1984 |
| Description | The design methodology used in the HiMAT program and the wind tunnel development activities are discussed. Selected results from the flight test program are presented and the strengths and weaknesses of testing advanced technology vehicles using the RPV concept is examined. The role of simulation on the development of digital flight control systems and in RPV's in particular is emphasized. |
| File Size | 6466162 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850006527 |
| Archival Resource Key | ark:/13960/t9770b17t |
| Language | English |
| Publisher Date | 1984-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Flight Tests Performance Tests Systems Engineering Aerospace Technology Transfer Wind Tunnel Tests Aerodynamics Digital Command Systems Highly Maneuverable Aircraft Remote Control Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
