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... ; title = Mikhail Tyurin titlestyle = image = Image:Astronaut_tyurin.jpg 200px imagestyle = caption = Mikhail Tyurin captionstyle = headerstyle = background: ccf; labelstyle = background: ddf; datastyle = text-align:right; header1 = label1 = data1 = header2 = label2 = Birth Name data2 = Mikhail Tyurin header3 = label3 ... = label7 = Occupation data7 = Russian Cosmonaut label8 = Nationality data8 = label9 = Notable Works data9 = Personal Data Michael Tyurin lives in Korolev, a small city outside of Moscow. He was born March 2, 1960 ...

REDIRECT Mikhail Tyurin Category:Astronaut-Cosmonaut

... Infobox bodystyle = float:right; valign:top; title = Mikhail Borisovich Kornienko titlestyle = image = Image:Astronaut_kornienko.jpg 200px imagestyle = caption = Mikhail Borisovich Kornienko captionstyle = headerstyle = background: ccf; labelstyle = background: ddf; datastyle = text-align:right; header1 = label1 = data1 = header2 = label2 = Birth Name data2 = Mikhail Borisovich Kornienko header3 = label3 = Birth Date data3 = 0Jan/05/Feb0JanMar 4 1960 header4 = label4 = Birth ...

... bureaus became known, such as Korolev, Chelomei, Mishin and Glushko. The least well known was Mikhail Klavdeivich Tikhonravov (1900- 74) partly because he sought little attention, partly because he lacked organizational ...

REDIRECT Mikhail Borisovich Kornienko Category:Astronaut-Cosmonaut

REDIRECT Mikhail K. Yangel Category:Engineer

REDIRECT Mikhail Tikhonravov Category:Engineer

... 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 ...

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