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From The Space Library
Displaying 1—10 of 1000 matches for query "LUNA_V" retrieved in 0.001 sec with these stats:
- "luna" found 476 times in 247 documents
- "v" found 3624 times in 2005 documents
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.
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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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