Into the Beyond: A Crewed Mission to a Near-Earth Object - NASA

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djk 9/20/07 . NEO Orion Configuration Overview The Orion’s ∂ V capability post-LEO escape is ~1.7 km/sec. Into the Beyond: A Crewed Mission to a Near-Earth Object :: International Astronomical Congress 2007 CONSTELLATION NEO Science Payload Bay (same as the Proposed Lunar Science Bay) 12
djk 9/20/07 . EELV for Launch of Earth Escape Stage • Atlas V Heavy Lift Vehicle – “Maximum” capability to 100x100 nmi: 64.9 klb – Centaur wet mass: 50.6 klb – Launch vehicle margin: 22% • Delta IV Heavy has marginal capability for orbiting a fully loaded Centaur. • Both launch vehicle lines have more capable versions on the drawing board. Into the Beyond: A Crewed Mission to a Near-Earth Object :: International Astronomical Congress 2007 Centaur as a payload for Atlas V HLV CONSTELLATION 13
Page 1 and 2: djk 9/20/07 . Into the Beyond: A Cr
Page 3 and 4: djk 9/20/07 . What is a NEO (Near E
Page 5 and 6: djk 9/20/07 . Example NEO Trajector
Page 7 and 8: NEO Population Discovery 2006: 3% K
Page 9 and 10: djk 9/20/07 . Precursor NEO Mission
Page 11: 110.6 meters Historical Ref Only dj
Page 15 and 16: djk 9/20/07 . “Upper Bookend” N
Page 17 and 18: djk 9/20/07 . Lower Bookend (Ares I
Page 19 and 20: djk 9/20/07 . Lower Bookend (Ares I
Page 21 and 22: NEO mission allows early checkout a
Page 23 and 24: Planned Robotic Missions to NEOs Cx
Page 25 and 26: djk 9/20/07 . Into the Beyond: A Cr
Page 27 and 28: djk 9/20/07 . Selecting a Target NE
Page 29: djk 9/20/07 . Summary Findings for

Into the Beyond: A Crewed Mission to a Near-Earth Object - NASA

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