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Displaying 1—10 of 1000 matches for query "Gennady_V._Sarafanov" retrieved in 0.001 sec with these stats:
- "gennadi" found 84 times in 71 documents
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- "sarafanov" found 11 times in 5 documents
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data2 = Gennady Mikhailovich Strekalov
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data3 = 0Feb/06/Feb0JanMar 10 1940
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... complex as part of an international Soviet-Indian crew comprised of Yu. V. Malishev, G. M. Strekalov, and R. Sharma, of India. In the period ...
Image:Gennadiy Vasiliyevich Sarafanov.jpg 200px
Gennadiy Vasiliyevich Sarafanov; Lieutenant Colonel; born January 1, 1942 near Saratov; married, two children.
Graduated from a higher military aviation school, and became a cosmonaut in 1965. He was the commander of Soyuz 15 .
:Category:Astronaut-Cosmonaut
REDIRECT
Gennadiy Vasiliyevich Sarafanov
Category:Astronaut-Cosmonaut
... ;
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data2 = Gennady Ivanovich Padalka
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data3 = Jun 21 1958
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data4 ... , Russia. Married to Irina Anatolievna Padalka (Ponomareva). They have three daughters, Yulia, Ekaterina and Sonya. Gennady enjoys the theater, parachute sport and diving.
Education
Graduated from Eisk Military Aviation College in ...
REDIRECT Gennady Ivanovich Padalka
Category:Astronaut-Cosmonaut
REDIRECT Gennady Mikhailovich Strekalov
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.
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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 ...
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