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

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•View from Behind Halo •Rendezvous: •∆V: 70.9 m/s •∆T: 4.5 days •Earth •Moon •Target at Ascent Time •Ascent: •∆V: 2.339 km/s •FPA: 75.6° •FPAz: 11.7° 24 24
•View from the Side •Earth •Ascent: •Moon •∆V: 2.339 km/s •FPA: 75.6° •FPAz: 11.7° •Rendezvous: •∆V: 70.9 m/s •∆T: 4.5 days 25 25
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 23: 2/25/2013 LUNAR ASCENT VEHICLE: ASC
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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