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Displaying 1—10 of 1000 matches for query "Kondakova,_Elena_V." retrieved in 0.001 sec with these stats:

  • "kondakova" found 20 times in 8 documents
  • "elena" found 50 times in 33 documents
  • "v" found 3624 times in 2005 documents



REDIRECT Elena V. Kondakova Category:Astronaut-Cosmonaut
... ; title = Elena V. Kondakova titlestyle = image = Image:Astronaut_kondakov.jpg 200px imagestyle = caption = Elena V. Kondakova captionstyle = headerstyle = background: ccf; labelstyle = background: ddf; datastyle = text-align:right; header1 = label1 = data1 = header2 = label2 = Birth Name data2 = Elena V. Kondakova header3 ...
REDIRECT Elena V. Kondakova
... Infobox bodystyle = float:right; valign:top; title = Elena Olegovna Serova titlestyle = image = Image:Astronaut_serova.jpg 200px imagestyle = caption = Elena Olegovna Serova captionstyle = headerstyle = background: ccf; labelstyle = background: ddf; datastyle = text-align:right; header1 = label1 = data1 = header2 = label2 = Birth Name data2 = Elena Olegovna Serova header3 = label3 = Birth Date data3 = Apr 22 1976 header4 = label4 = Birth Place data4 ...
REDIRECT Elena Olegovna Serova Category:Astronaut-Cosmonaut
... recover from the cancellation of the CF-105 project. On December 18th 1959 the A.V. Roe parent company, Hawker Siddeley, purchased De Havilland and began the consolidation of the two Canadian aircraft companies. A.V. Roe's Canadian Applied Research Applied Research Division was merged with De Havilland's Special ...
... Program (Phase One) Booster Feasibility Demonstration (13 October 1958) Media:1958-11-15 Juno V.pdf Juno V Space Vehicle Development Program (Status Report (15 November 1958) Media:1958-12 NASA ABMA.pdf ABMA Presentation to the NASA (15 December 1958) Media:1959-01-05 Juno V.pdf Juno V Transportation Feasibility Study (5 January 1959) Media:1959-05-01 ABMA Soft Lunar Landing ...
... performance military rockets can provide about 3300 feet per second of delta V. Space travel requires a very large delta V. The first objective of a launch to space is to get ... LEO from the Earth's surface requires about 30,000 feet per second of delta V. To escape the Earth's gravity field from LEO requires another 9,800 feet per ... . Landing on the Moon or other planets and returning home requires even more total delta V capability. ---- Answer provided by John W. Cole Image:K2S logosmall.jpg Question and Answer extracted ...
... Society for Volume 64 64 '''Page ''' - 204-213 '''Year''' - 2011 '''Keywords''' - Interplanetary trajectory, C3, delta-V, pork-chop plot, launch window, Mars, Venus flyby '''JBIS Reference Code ''' - 2011.64.204 '''Number ... which is capable of calculating ballistic interplanetary trajectories with planetary flyby options to create exhaustive V contour plots for both direct trajectories without flybys and flyby trajectories in a single chart ...
... Floyd V. Bennett - Interviewed by Jennifer Ross-Nazzal''' '''Houston, Texas – 22 October 2003 '''Ross-Nazzal:''' Today is ... our fellows on the console, Willis M. Bolt, Dan Joe D. Payne, and Jim James V. West and I’ve left someone out , Jim James H. Alphin. And they were in ...

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