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Mission data MissionTotal mission duration [d]Crew size [-] Total mission Δv [m/s] from LEO (including mid-course corrections) Lunar flyby843300 Low lunar.

Published byRobert Hawkins Modified over 8 years ago

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Presentation on theme: "Mission data MissionTotal mission duration [d]Crew size [-] Total mission Δv [m/s] from LEO (including mid-course corrections) Lunar flyby843300 Low lunar."— Presentation transcript:

1 Mission data MissionTotal mission duration [d]Crew size [-] Total mission Δv [m/s] from LEO (including mid-course corrections) Lunar flyby843300 Low lunar orbit1045000 SE-L2 visit6045100 GEO visit4546000 (including 28.5° plane change) NEO visit (minimalist)18027100

2 Launch vehicle data OptionSolid Rocket BoostersCore StageLEO Payload [kg]Source 1 2 x 4-Segment Solid Rocket Boosters 3 x SSME, Side- Mounted 71 Presentation to the Augustine Committee 2 2 x 4-Segment Solid Rocket Boosters 3 x SSME, Inline74ESAS Report 3 2 x 5-Segment Solid Rocket Boosters 4 x SSME, Inline97ESAS Report

3 Mission payloads MissionCEV Block II Upgraded CEV Block II LSAM crew compartment Additional consumables Science payload Total payload Lunar flyby10797 kg---1000 kg11797 kg Low lunar orbit 10797 kg---1000 kg11797 kg SE-L2 visit-11379 kg2455 kg600 kg4000 kg18434 kg GEO visit-11379 kg2455 kg0 kg4000 kg17834 NEO visit (minimalist) -11379 kg2455 kg1800 kg500 kg16134 kg

4 Delta 4 Heavy US CEV SM + 1 Delta 4 Heavy Upper Stage CEV SM + 2 Delta 4 Heavy Upper Stage CEV SM + 3 Delta 4 Heavy Upper Stage CEV SM + 4 Delta 4 Heavy Upper Stage CEV SM + 5 Delta 4 Heavy Upper Stage 2 x [3 SSME + 2 x 4-Segment SRB, Inline] 2 x [4 SSME + 2 x 5-Segment SRB, Inline] 2 x [3 SSME + 2 x 4-Segment SRB, Side-Mount] 1 x [4 SSME + 2 x 5-Segment SRB, In-line] 1 x [3 SSME + 2 x 4-Segment SRB, Inline] 1 x [3 SSME + 2 x 4-Segment SRB, Side-Mount] 1 x [4 SSME + 2 x 5-Segment SRB, In-line] Low Lunar Orbit Mission (4 Crew) SE-L2 Mission (4 Crew) Lunar Flyby Mission (4 Crew) GEO Mission (4 Crew) NEO Mission (2 Crew)

5 Centaur V1 CEV SM + 1 Centaur V1 CEV SM + 2 Centaur V1 CEV SM + 3 Centaur V1 CEV SM + 4 Centaur V1 CEV SM + 5 Centaur V1 2 x [3 SSME + 2 x 4-Segment SRB, Inline] 2 x [4 SSME + 2 x 5-Segment SRB, Inline] 2 x [3 SSME + 2 x 4-Segment SRB, Side-Mount] 1 x [3 SSME + 2 x 4-Segment SRB, Inline] 1 x [4 SSME + 2 x 5-Segment SRB, In-line] 1 x [3 SSME + 2 x 4-Segment SRB, Side-Mount] 1 x [4 SSME + 2 x 5-Segment SRB, In-line] Low Lunar Orbit Mission (4 Crew) SE-L2 Mission (4 Crew) Lunar Flyby Mission (4 Crew) GEO Mission (4 Crew) NEO Mission (2 Crew)

6 ITV Designs 2 x 4-Segment Solid Rocket Boosters + 3 x SSME Side- Mount OR 2 x 4-Segment Solid Rocket Boosters + 3 x SSME In-Line Launch 1 Launch 2 2 x 5-Segment Solid Rocket Boosters + 4 x SSME In-Line Launch 1 Launch 2 CEV Centaur V1 ~ 30 m Crew compartment + Science Payload Centaur V1 ~ 25 m CEV Delta IV Heavy Upper Stage ~ 25 m Crew compartment + Science Payload Delta IV Heavy Upper Stage

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