Mission data
description
Transcript of Mission data
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Mission data
MissionTotal missionduration [d]
Crewsize [-]
InjectionΔv [m/s]
Destination capture
Δv [m/s]
Destinationdeparture
Δv [m/s]
Lunar flyby 7 (3.5/0/3.5) 4 3200 20 (MCC) 20 (MCC)
Lunar orbit 9 (3.5/2/3.5) 4 3200 835 + 20 (MCC) 835 + 20 (MCC)
SE-L2 visit 80 (35/10/35) 4 3200 400 + 50 (MCC) 400 + 50 (MCC)
GEO visit 10.5 (0.25/10/0.25) 4 24302100 (incl. 28.5° plane change)
1470
NEO visit 138 (111/16/11) 3 3291 2193 1746
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Science Payloads
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Consumables data
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Habitable volume
Orioncrew module
LSAMcrew module
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Launch vehicle data
Option Solid Rocket Boosters Core Stage LEO Payload [kg] Source
12 x 4-Segment Solid
Rocket Boosters3 x SSME, Side-
Mounted72000
Presentation to the Augustine Committee
22 x 4-Segment Solid
Rocket Boosters3 x SSME, Inline 74000 ESAS Report
32 x 5-Segment Solid
Rocket Boosters4 x SSME, Inline 97000 ESAS Report
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Launch vehicle shroud volume
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Mission payloads
Mission CEV Block IIUpgraded
CEV Block IILSAM crew
compartmentAdditional
consumablesScience payload
Total payload
Lunar flyby 10797 kg - - - 1650 kg 12847 kg
Lunar orbit 10797 kg - - - 1650 kg 12847 kg
SE-L2 visit - 11379 kg 2455 kg 1301 kg 4196 kg 19731 kg
GEO visit - 11379 kg 2455 kg 0 kg 4196 kg 18430 kg
NEO visit - 11379 kg 2455 kg 2175 kg 1476 kg 17685 kg
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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]
Lunar Orbit
SE-L2
Lunar Flyby
GEO
NEO
1 x [4 SSME +2 x 5-Segment SRB,
In-line]
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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
Lunar Orbit
SE-L2
Lunar Flyby
GEO
NEO
1 x [3 SSME +2 x 4-Segment SRB,
Inline]
2 x [4 SSME +2 x 5-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]
2 x [3 SSME +2 x 4-Segment SRB,
Inline]
2 x [3 SSME +2 x 4-Segment SRB,
Side-Mount]
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Numerical C3 analysis
4 Centaur V1 stages3 Centaur V1 stages
2 Centaur V1 stages
1 Centaur V
1 stage
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Lunar Flyby Mission Storyboard
Earth
Lunarorbit
LEO
Earth’smoon
Centaur V1 stages discarded
Launch 1
Trans-lunar coast Trans-Earth coast
Earth entry
Earth landing
Lunar flyby
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Lunar Orbit Mission Storyboard
Earth
Lunarorbit
LEO
Earth’smoon
Centaur V1 stages discarded
Launch 1
Trans-lunar coast Trans-Earth coast
Earth entry
Earth landing
Lunar orbit operations
Science package discarded
Low lunar orbit capture Low lunar orbit departure
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SE-L2 Mission Storyboard
Earth
SE-L2halo orbit
LEO
SE-L2asset
Centaur V1 stages discarded
Launch 1
Trans-SE-L2 coast Trans-Earth coast
SE-L2 captureSE-L2 departure
SE-L2operations
Earth entry
Earth landing
Servicing payload left atthe observation asset
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SE-L2 Earth departure
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GEO Mission Storyboard
Earth
GEO
LEO
Centaur V1 stages discarded
Launch 1 Launch 2
Trans-GEO coast Trans-Earth coast
GEO capture
GEO departure
GEO operations
Earth entry
Earth landing
GEOasset
Mission module and sciencepayload discarded
Capture stage discarded
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GEO Mission GEO insertion
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NEO Mission Storyboard
Earth
NEOvicinity
LEO
NEO
Centaur V1 stages discarded
Launch 1 Launch 2
Trans-NEO coast Trans-Earth coast
NEO capture
NEO departure
NEO exploration
Earth entry
Earth landing
Capture stage discarded
Mission module and sciencepayload discarded
Consumables for trans-NEO coast discarded
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NEO Mission – NEO Insertion