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Apollo lunar module landing gear
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Rogers, W. F. |
| Copyright Year | 1972 |
| Description | The Apollo lunar module landing-gear flight-performance results and three principal gear development problems are discussed. In evaluating the lunar module touchdown performance, strut stroking and toppling stability are the prime factors and are governed primarily by touchdown velocity and surface slope at the touchdown point. Flight results are shown to be well within design values, and the landing-gear has performed successfully in all landings. |
| File Size | 444819 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730010151 |
| Archival Resource Key | ark:/13960/t02z60j10 |
| Language | English |
| Publisher Date | 1972-11-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Performance Tests Statistical Analysis Structural Stability Landing Gear Thermal Insulation Struts Touchdown Lunar Module Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
