Touchdown Dynamics Analysis of Spacecraft for Soft Lunar Landing
Author | : Robert E. Lavender |
Publisher | : |
Total Pages | : 48 |
Release | : 1964 |
Genre | : Lunar excursion module |
ISBN | : |
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Author | : Robert E. Lavender |
Publisher | : |
Total Pages | : 48 |
Release | : 1964 |
Genre | : Lunar excursion module |
ISBN | : |
Author | : Robert E. Lavender |
Publisher | : |
Total Pages | : 68 |
Release | : 1965 |
Genre | : Lunar surface vehicles |
ISBN | : |
Results of analytical touchdown dynamics investigations are presented which were conducted to obtain estimates of the probability of stable landing for configurations with various landing gear diameters. Both three-legged and four-legged vehicles are considered in the analysis. Dynamic scaling considerations are taken into account so that the results are applicable to a wide range of vehicle size and mass. A Monte Carlo approach is taken in the determination of initial landing conditions. Results indicate that for a given probability of stable landing, a three-legged vehicle requires a landing gear diameter only slightly larger than the diameter required for a four-legged vehicle. Therefore the three-legged vehicle's landing gear should weigh less.
Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 1152 |
Release | : 1965 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1504 |
Release | : 1979 |
Genre | : United States |
ISBN | : |
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1194 |
Release | : 1966-07 |
Genre | : Government publications |
ISBN | : |