Add to ORKGDigital computer techniques applied to study of impact dynamics of lunar landing vehicle
The Apollo lunar module landing-gear flight-performance results and three principal gear development...
An experimental investigation has been made of some lunar-landing characteristics of a 1/6-scale dyn...
Monte Carlo method for determination of touchdown dynamics for soft lunar landin
Full scale dynamic landing impact investigation of prototype lunar module landing gea
Dynamic scale model of lunar module type spacecraft - overturn stability for nonlevel surface landin...
Mathematical prediction model for landing dynamics of impacting struts, and trusses of lunar vehicle...
Trajectory requirements for terminal lunar landing from analog simulation of spacecraf
Computer programs perform landing stability studies of mechanical impact system designs for advanced...
Technique for conducting landing impact tests at simulated planetary gravity for Mars lander spacecr...
Optical simulation study to determine manual instrumentation for pilot control of lunar flying vehic...
An investigation of a 1/6-scale dynamic model has been made to develop and evaluate a technique for ...
The safe landing of a Moon lander and the performance of the precise instruments it carries may be a...
The initial demonstration model of a lunar base simulation is described. This initial model was deve...
Apollo spacecraft landing simulation to determine impact water pressures, accelerations, and landing...
EagleCam is a pico-satellite (CubeSat) with dimensions of 100 x 100 x 150 mm3 that is going to the m...
The Apollo lunar module landing-gear flight-performance results and three principal gear development...
An experimental investigation has been made of some lunar-landing characteristics of a 1/6-scale dyn...
Monte Carlo method for determination of touchdown dynamics for soft lunar landin
Full scale dynamic landing impact investigation of prototype lunar module landing gea
Dynamic scale model of lunar module type spacecraft - overturn stability for nonlevel surface landin...
Mathematical prediction model for landing dynamics of impacting struts, and trusses of lunar vehicle...
Trajectory requirements for terminal lunar landing from analog simulation of spacecraf
Computer programs perform landing stability studies of mechanical impact system designs for advanced...
Technique for conducting landing impact tests at simulated planetary gravity for Mars lander spacecr...
Optical simulation study to determine manual instrumentation for pilot control of lunar flying vehic...
An investigation of a 1/6-scale dynamic model has been made to develop and evaluate a technique for ...
The safe landing of a Moon lander and the performance of the precise instruments it carries may be a...
The initial demonstration model of a lunar base simulation is described. This initial model was deve...
Apollo spacecraft landing simulation to determine impact water pressures, accelerations, and landing...
EagleCam is a pico-satellite (CubeSat) with dimensions of 100 x 100 x 150 mm3 that is going to the m...
The Apollo lunar module landing-gear flight-performance results and three principal gear development...
An experimental investigation has been made of some lunar-landing characteristics of a 1/6-scale dyn...
Monte Carlo method for determination of touchdown dynamics for soft lunar landin