Loading...
Please wait, while we are loading the content...
Similar Documents
Wind tunnel pressure signatures for a .016 scale model of the apollo command module
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mendoza, J. P. Hicks, R. M. |
| Copyright Year | 1971 |
| Description | Pressure signatures were measured at roll angles ranging from 0 to 180 deg for a .016-scale model of the Apollo Command Module spacecraft at 25 deg angle of attack. The test Mach numbers ranged from 1.50 to 10.02. |
| File Size | 14261085 |
| Page Count | 46 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730005178 |
| Archival Resource Key | ark:/13960/t4cp1vt8j |
| Language | English |
| Publisher Date | 1971-07-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Pressure Distribution Wind Tunnel Models Roll Angle of Attack Apollo Spacecraft Command Modules Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
