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Displaying 1—10 of 1000 matches for query "Parametric_Analysis_for_Aurora_Mars_Manned_Mission_Concept_Definition" retrieved in 0.015 sec with these stats:
- "parametr" found 20 times in 13 documents
- "analysi" found 2321 times in 1516 documents
- "for" found 102366 times in 17182 documents
- "aurora" found 386 times in 258 documents
- "mar" found 48386 times in 4487 documents
- "man" found 10979 times in 4195 documents
- "mission" found 32560 times in 9616 documents
- "concept" found 2924 times in 1581 documents
- "definit" found 947 times in 731 documents
... of the Aurora program (ESA program), Europe plans to get its own vision about future Mars manned mission. Within this context, we have performed an end-to-end analysis of what could be these missions, focusing ... be a no Mars infrastructure deployment and a single spacecraft going to Mars and returning back to Earth. But it implies for the crew to stay in Mars orbit several months, waiting for the ...
... for their day.
Yet, it was also realized even during the preliminary collecting of material on these kinds of concepts that a two-part survey would still not result in a genuinely “definitive ... to find this topic fascinating and worthy of continued exploration. Searches for other examples of reaction-propulsion concepts for manned flying machines was therefore further pursued, as well as efforts ...
... - Contents of the Journal of the British Interplanetary Society for Volume 59 59
'''Page ''' - 313-318
'''Year''' - 2006
'''Keywords''' - Mars habitats, ISRU, glass
'''JBIS Reference Code ''' - 2006. ... the entire habitat from local materials is unfeasible for early missions, this design can be implemented during the very first manned mission. The proposed habitat will have a cylindrical ...
Media:19750069405_1975069405.pdf Apollo Extension Systems For Continuous Earth Orbit Missions (7MB PDF)
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
... Fission Power System (FPS) for future unspecified National Aeronautics and Space Administration (NASA) science missions. FPS technology was considered a potential option for power levels that might ... . After completing a short round of concept screening studies, the team selected a single concept for concentrated study and analysis. The selected concept is a solid block uranium-molybdenum ...
... .jpg Lockheed design for six-man Apollo landing stage (1968)
Image:Lockheed6manLander.jpg Lockheed design for six-man Apollo landing stage (1968)
Image:Lockheed 6manApolloERS.jpg Lockheed design for Earth Return Stage for six-man Apollo (1968)
Image:Lockheed 6manApolloCSM.jpg Lockheed design for CSM for six-man Apollo with ...
... .386
'''Number of Pages''' - 9
Abstract
In this paper some potentially interesting transfer options for missions to Near Earth Objects have been studied. Due to the high number of potential targets and to the large variety of possible missions that can be considered, especially if resorting to low-thrust propulsion, an extensive analysis of transfer options requires a preliminary approach ...
... of the Journal of the British Interplanetary Society for Volume 60 60
'''Page ''' - 202-208
'''Year''' - 2007
'''Keywords''' - Bepi-Colombo, interplanetary trajectory design, mission analysis, Mercury, low-thrust
'''JBIS Reference Code ''' - 2007.60.202
'''Number of Pages''' - 7
Abstract
BepiColombo will be the first European mission to Mercury and the first mission ever to use ...
... . Lorenz
'''Co-Author(s)''' -
'''JBIS Volume ''' - Contents of the Journal of the British Interplanetary Society for Volume 53 53
'''Page ''' - 218-234
'''Year''' - 2000
'''Keywords''' -
'''JBIS Reference Code ''' - 2000.53.218 ...
The likely scientific questions posed by Titan after the upcoming Cassini mission, and the engineering issues associated with the platforms required for these investigations, are reviewed. Landers and balloons satisfy a limited ...
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