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Displaying 81—90 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 MSG Central Facility, being developed by Science Systems for EUMETSAT1, represents the first of a new generation of satellite mission control systems, based on the Windows NT operating system. The system makes use of a range of new technologies to provide an integrated environment for the planning, scheduling, control and monitoring of the entire ...
... - A. Bolonkin '''Co-Author(s)''' - '''JBIS Volume ''' - Contents of the Journal of the British Interplanetary Society for Volume 56 56 '''Page ''' - 231-249 '''Year''' - 2003 '''Keywords''' - Space transport system, space elevator, Mars transport system, Moon transport system, Employ- ment of asteroids. '''JBIS Reference Code ''' - 2003.56.231 '''Number of ...
... of finding the true anomaly given the time of flight and the periapsis distance, particularly for short times of flight presents significant difficulties. These difficulties involve the preservation of the numerical accuracy of the solution of the cubic equation for the true anomaly . Here a solution for ...
... presents the design of the overall trajectory, starting from a highly eccentric Earth orbit up to the polar orbits of the MMO (Mercury Magnetospheric Orbiter, JAXA) and the MPO (Mercury Planetary Orbiter, ESA). Results for the interplanetary trajectory optimisation, including the lunar flyby design, as well as the ...
... of Energy (DOE) team is developing concepts and technologies for affordable nuclear Fission Power Systems (FPSs) to support future exploration missions. A key deliverable is the Technology Demonstration Unit (TDU). The TDU will assemble the major elements of a notional FPS with a non-nuclear ...
... -metallics such as Kevlar and epoxy are also used for such things as stowage lockers. The thermal protection system, or heat shield, uses a range of heat-resistant materials such as carbon, alumina, silicon, silicon carbide, and aramids to make insulation blankets and tiles. (Ref. 1) Ref 1.NASA, National Space Transportation System Reference, Volume 1 Systems ...
... for the astronauts. The spacesuit that the astronauts wear during launch and also during re-entry and landing is the ACES. Each ACES costs about $150,000, and that includes everything from the helmet to the boots. The company that makes the EMU suit (ILC Dover) says that it is difficult to express the cost of the suit. It has been reported in the news media that the ...
... with the solar wind of the interstellar medium. This is called the termination shock. However, most astronomers agree that there is a great swarm of comets around our solar system. The far edge of this ... extracted from the book Kids to Space - by Lonnie Schorer Image:9781894959421.jpg '''Buy This Book''' http://www.apogeebooks.com/Books/For%20Kids/KidstoSpace.html ...
... a quaternion is mentioned, it is implied to be a quaternion of rotation, which can thus be done without loss of generality. A useful expression for the quaternion comes from the fact that it can be parameterized by a ... taking Eq. (II.16) as the dynamics equation, the response of the SC to a reaction wheel command becomes substantially easier to model. An Accurate, Inexpensive Attitude Determination and Control System for CubeSats by Duarte Rondão, Cass ...
... system has not yet been simulated. The truth model dynamics are ruled by Eqs. (II.9) and (II.16), as presented in Section II. Table 6 displays the general model parameters used for the ...

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