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Image:Luna9.jpg 300px Luna IX schematic Image:Luna9engine.jpg 300px Closed loop engine used for Luna 9 mission Image:Luna9mockup.jpg 300px Luna IX ALS mockup at Energia museum Image:Luna9payload1.jpg 300px Luna IX pennants delivered to the moon Image:Luna9pennants2.jpg 300px Luna IX pennant delivered to the moon Category:Spacecraft

Image:LunaIprobe.jpg 300px Luna I probe Image:Luna1Estage.jpg 300px Luna I probe inside E Stage Image:Luna1launcher.jpg 300px Luna I probe and E stage on R-7 booster Category:Spacecraft

Image:Luna2.jpg 300px Luna II probe Image:Luna2mockup.jpg 300px Luna II mockup at Energia museum Image:Luna2payload.jpg 300px Luna II pennants delivered to moon's surface Category:Spacecraft

Image:Luna3.jpg 300px Luna III probe Image:Luna3mockup.jpg 300px Luna III mockup at Energia museum Category:Spacecraft

REDIRECT Luna 10

REDIRECT Luna 10

... 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 ...

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