A Study of Abort from a Manned Lunar Landing and Return to Rendezvous in a 50-mile Orbit PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download A Study of Abort from a Manned Lunar Landing and Return to Rendezvous in a 50-mile Orbit PDF full book. Access full book title A Study of Abort from a Manned Lunar Landing and Return to Rendezvous in a 50-mile Orbit by Jack A. White (NASA researcher.). Download full books in PDF and EPUB format.
Author: Jack A. White (NASA researcher.) Publisher: ISBN: Category : Aborted missions Languages : en Pages : 24
Book Description
"An investigation has been made of some of the problems associated with abort from landing and return to an orbiting vehicle in a 50-mile lunar orbit. For this study the landing module was considered capable of direct return to the orbiting vehicle from a hovering position at the lunar surface. The investigation was divided into two parts, an analytical study and a simulation study. The results of the analytical study indicate that, for an economical return to the orbiting vehicle, the landing maneuver should be chosen such that the orbiting vehicle is almost directly above the landing module at the touchdown point. This requirement places limitations on the angular travel of the landing vehicle around the moon prior to touchdown. Results of the simulation study indicate that a pilot can control the abort maneuver by using visual information."--Summary.
Author: Jack A. White (NASA researcher.) Publisher: ISBN: Category : Aborted missions Languages : en Pages : 24
Book Description
"An investigation has been made of some of the problems associated with abort from landing and return to an orbiting vehicle in a 50-mile lunar orbit. For this study the landing module was considered capable of direct return to the orbiting vehicle from a hovering position at the lunar surface. The investigation was divided into two parts, an analytical study and a simulation study. The results of the analytical study indicate that, for an economical return to the orbiting vehicle, the landing maneuver should be chosen such that the orbiting vehicle is almost directly above the landing module at the touchdown point. This requirement places limitations on the angular travel of the landing vehicle around the moon prior to touchdown. Results of the simulation study indicate that a pilot can control the abort maneuver by using visual information."--Summary.
Author: United States. Department of Commerce. Office of Technical Services Publisher: ISBN: Category : Government publications Languages : en Pages : 836
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division Publisher: ISBN: Category : Aeronautics Languages : en Pages : 262
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Publisher: ISBN: Category : Aeronautics Languages : en Pages : 258
Author: Jack A. White (NASA researcher.)
Author: Jack A. White (NASA researcher.)
Author: 
Author: 
Author: United States. Department of Commerce. Office of Technical Services
Author: United States. Superintendent of Documents
Author: 
Author: 
Author: United States. Superintendent of Documents
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division