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Displaying 31—40 of 1000 matches for query "A_Survey_Of_Various_Vehicle_Systems_For_The_Manned_Lunar_Landing_1961" retrieved in 0.057 sec with these stats:
- "a" found 169938 times in 18149 documents
- "survey" found 1708 times in 1097 documents
- "of" found 295472 times in 20552 documents
- "various" found 1803 times in 1215 documents
- "vehicl" found 10011 times in 4664 documents
- "system" found 26638 times in 8217 documents
- "for" found 102366 times in 17182 documents
- "the" found 506431 times in 20587 documents
- "man" found 10979 times in 4195 documents
- "lunar" found 12612 times in 4514 documents
- "land" found 10467 times in 4286 documents
- "1961" found 12306 times in 1330 documents
... The paper considers several future missions, the landing requirements produce different thrust level needed for the landing vehicle but are similar in many other repects. To fulfil the mission needs of these planetary lander studies, preferably with a ...
... process the raw results to create survey location maps for the subject of the survey. Such surveys are conducted for a location or region and referenced to the earth global co- ordinate system with global positioning system (GPS) positioning. Due to this referencing the survey is only as accurate as the ...
Media:Army Lunar commprobrelaluna_022807133241.pdf Comments on Problems Relating to the Lunar Landing Vehicle US Army 1958 (37MB PDF)
Category:Publications
... lunar settlement
'''JBIS Reference Code ''' - 2005.58.131
'''Number of Pages''' - 7
Abstract
Several reasons for going back to the Moon are listed: scientific study of our natural satellite, Earth and in general the Solar System; exploitation of the ...
... systems to become viable for spacecraft in this category. The paper therefore considers initially the application of EP systems to a variety of future missions, the benefits achieved by the use of this technology, and the various thruster types which are suitable for ...
... of Pages''' - 13
Abstract
A crewless reusable vertical take-off horizontal landing space transportation system is investigated. The single stage launch vehicle goes into a very low orbit around the Earth. At burnout, the payload is deployed. At apogee, the ...
... the number of vehicles, the trajectory V, and the crew mission duration. The trajectory V drives propulsion system require- ments and the mission duration affects the crew's health. One-, two-, and three-vehicle scenarios are presented for the colonization of ...
... a serious threat to our civilization and its ecological support systems. Ideally this problem will be overcome by reducing greenhouse gas emissions. Various ... of micron-sized dust particles derived from comet fragments or lunar mining, and positioned in orbits near the triangular Lagrange points of the Earth-Moon system. Solar radiation pressure can render such orbits unstable, but a class of ...
... FOR THE DESIGN OF MISSILES'''
by Various
''Cambridge (Massachusetts), 1948: Harvard University Press, 226 pages, OP''
Prepared by the staff of the Harvard Computation Laboratory, the book is a collection of tables useful to the designer of guided missiles.
Extracted from the ...
... FOR THE MOON'''
by Caidin, M.
''New York, 1959: E. P. Dutton Co., Inc., 285 pages, $4.95''
The nature of the Moon, lunar probing, details of US and Soviet lunar probe vehicles ...
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