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Image:GMlunarrover1962.jpg 400px General Motors Six-Wheel Flexible Frame Lunar Rover (ca. 1961) Image:GMLunarRover.jpg 300px General Motors Defense Systems Division design for a lunar roving vehicle, (ca. November 1961) Category:Lunar Vehicles

... 300px A hypothetical four-stage chemical-rocket propelled space vehicle is pictured as it might appear carrying an eight-man crew on a round trip ... satellite orbits. The structure at left is the detachable quarters and the chemical rocket vehicle for soft landing and exploration of Mars. This chemical spaceship is designed to operate in a gravity ...

... RESEARCH''' by Bijl, H. K. Kallman (ed) ''Amsterdam, 1960: North- ... of the Ionosphere on Signals from Earth Satellites," "Radio Propagation between Space Vehicle and The Earth in the Presence of the Ionosphere," "The ... Field Instrumentation and Measurements," "Cosmic Ray Investigation by the Second Cosmic Rocket Landed on the Moon," "Soft Radiation Measurements on Explorer VI Earth Satellite," ...

I would think that in the near future re-entry of space vehicles will primarily be unpowered after the deorbit burn, because it eliminates a variable and it ... flexibility. Future vehicles will probably have the capability of providing some sort of propulsive thrust in case there is a problem making the runway or in case the landing location needs to ... /For%20Kids/KidstoSpace.html Click here Category:Kids To Space Category:Kids To Space - LANDING

... Launch Vehicle (CLV), which will be used to launch astronauts to low earth orbit and rendezvous with either the International Space Station or the ESMD's earth departure stage for lunar or other future missions beyond low Earth orbit. The primary elements of the Ares I CLV project are the first stage, the upper stage, the upper stage engine, and vehicle integration. Within vehicle integration is an effort in integrated design and analysis which is comprised of a ...

Media:19700076559_1970076559.pdf LANDING CHARACTERISTICS OF AN APOLLO-TYPE VEHICLE (2.5MB PDF) Category:Publications

... '''Number of Pages''' - 6 Abstract A recoverable Orbital Launch Vehicle is proposed configured along the lines of a commercially successful, expendable launch vehicle. The reuseable lower stage is comprised of a single ... in such a way so that each part is capable of surviving the impact of landing upon the ocean's surface, thus solving the paramount problem to reuseability. '''To BUY this ...

Media:1959-06 Lunar Research Flights AD0425380.pdf A Study Of Lunar Research Flights by Armour Research Foundation June 1959 Category:Publications

Media:1959ABMALunarPlan.pdf Army Ballistic Missile Agency Lunar Soft Landing Study (December 1959) Category:Publications

Media:1960-02_Weight_Advantages_of_Use_of_Parking_Orbit.pdf Weight Advantages of Use of Parking Orbit for Lunar Soft Landing Mission by William Michael (February 1960) Category:Publications

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