ORION/MOONRISE: JOINT HUMAN-ROBOTIC LUNAR SAMPLE RETURN MISSION CONCEPT

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2/25/2013 <strong>SAMPLE</strong> <strong>RETURN</strong> VEHICLE: DESCENT LEAG 2012: Orion/MoonRise 20 20 20
•3 month low-energy transfer to the Moon •Staging at L 1 or L 2 •7.5 day descent, which may begin before humans arrive at L 2 •Earth •Human MoonRise Mission •Moon-centered Viewed from the Side •Landing: •DV: 2.335 km/s, FPA: -7.0 deg, FPAz: -23.3 deg 21 21
Page 1 and 2: ORION/MOONRISE: JOINT HUMAN-ROBOTIC
Page 3 and 4: 3 Orion/MoonRise Mission Concept: I
Page 5 and 6: Addresses key objectives for Planet
Page 7 and 8: Launch together Cruise together (Ap
Page 9 and 10: 9 •EML2 Orbit Lunar Surface •EM
Page 11 and 12: 11 •2x ATK/PSI 80512 Tanks • 49
Page 13 and 14: 13 MoonRise Lander: Workspace chara
Page 15 and 16: Scenario Orion/MoonRise Mission Des
Page 17 and 18: •3 month low-energy transfer to t
Page 19: •3 month low-energy transfer to t
Page 23 and 24: 2/25/2013 LUNAR ASCENT VEHICLE: ASC
Page 25 and 26: •View from the Side •Earth •A
Page 27 and 28: •View from Earth •Target at Asc
Page 29 and 30: 29 The MoonRise arm provides a her
Page 31 and 32: Nation/ Institution ISS Partners Or
Page 33: ORION/MOONRISE: JOINT HUMAN-ROBOTIC

ORION/MOONRISE: JOINT HUMAN-ROBOTIC LUNAR SAMPLE RETURN MISSION CONCEPT

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