Loading...
Please wait, while we are loading the content...
Similar Documents
Effect of yaw angle on steering forces for the lunar roving vehicle wheel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Green, A. J. |
| Copyright Year | 1974 |
| Description | A series of tests was conducted with a Lunar Roving Vehicle (LRV) wheel operating at yaw angles ranging from -5 to +90 deg. The load was varied from 42 to 82 lb (187 to 365 N), and the speed was varied from 3.5 to 10.0 ft/sec (1.07 to 3.05 m/sec). It was noted that speed had an effect on side thrust and rut depth. Side thrust, rut depth, and skid generally increased as the yaw angle increased. For the range of loads used, the effect of load on performance was not significant. |
| File Size | 5131146 |
| Page Count | 63 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750021903 |
| Archival Resource Key | ark:/13960/t6p02z456 |
| Language | English |
| Publisher Date | 1974-10-01 |
| Access Restriction | Open |
| Subject Keyword | Lunar And Planetary Exploration Skidding Lunar Roving Vehicles Steering Vehicle Wheels Yaw Loads Forces 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 |
