THE ARTEMIS PROJECT
PRIVATE ENTERPRISE ON THE MOON
Reference Mission
Section 4.1.1.
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Options for Each Stage of the Reference Mission
Italicized
options are ones not likely to be used.
Launch Lunar Transfer Vehicle with its fuel
Key options:
Choice of
launcher
Separate launches for
LTV
and fuel
Send small robot cameras to moon ahead of manned vehicles
Check out the LTV
Key options:
Check out while attached to space station
Earth orbit flight
Circumlunar flight
Launch descent stage, ascent stage with fuel
Key options:
Choice of
launcher
Man-assisted assembly to LTV vs. automated rendezvous & dock
Launch
lunar base core module
Key options:
Choice of
launcher
Crew goes up with hab vs. separate launch
Choice of
crew transport
to low Earth orbit
Size of crew (
2
, 3, 4,
5, 6
)
Integrate and check out the Artemis stack in low Earth orbit
Key options:
At International Space Station
At Mir
At
Shuttle
Without assistance from other spacecraft
From our own transportation node in low Earth orbit (there goes the budget . . .)
Artemis stack trans-lunar injection
Key options:
Free return trajectory
Direct trajectory
Fuzzy boundary trajectory (not a viable option for manned flight)
Lunar orbit insertion
Key options:
Free return trajectory
Descent orbit trajectory for whole stack vs. separation
Choice of landing site
Undock and separate
Key options:
Manned
vs. automated
lunar transfer vehicle
Size of landing crew
No orbiting vehicle
Descent orbit initiation
Key options:
Drop automated cameras with landing beacons ahead of manned craft
Separate before or after DOI
Meanwhile, lunar transfer vehicle circularizes its orbit around moon
Key options:
Altitude
Descent
Key options:
Orbit tracking techniques
Landing beacons on surface
Inertial navigation
Star tracker and lunar map navigation
Doppler shift at ground stations for navigation
Earth-based radar navigation
Landing
Key options:
Choice of landing site
Amount of fly-around capability
Terrain roughness design specification
Methods of photographing the landing
Our own little cameras
Robot rovers
(
Carnegie-Mellon
)
Lunar Surface Operations
Key options:
Length of stay
Site survey
Low-g demonstrations
Geological investigations
Equipment for lunar traverse (feet, cart, rover)
Lunar mining pilot plant
Lunar oxygen pilot plant
Amount of material to harvest
Type of material to harvest
Ascent stage liftoff
Key options:
Size of landing crew
Weight of material to return
Pressurized
vs. unpressurized ascent stage
Ascent Stage + LTV rendezvous
Key options:
Choice of active vehicle (
LTV
or ascent stage)
Type of rendezvous equipment (rndz radar?)
Type of docking equipment
Transearth Injection
Key options:
Drop ascent stage
vs. keep it for re-use
Drop tanks used to get here
Earth orbit rendezvous
Key options:
Rockets
Aerobrake
Earth atmospheric entry
(probably not viable for Artemis)
Rendezvous with ISS
Rendezvous with Mir
Rendezvous with
Shuttle
Rendezvous with our own Earth orbit transportation node ($!)
Rendezvous with other spacecraft
Return crew and material to Earth surface
Key options:
Choice of spacecraft
Reference Mission
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ASI W9600461r1.1.
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Author:
Gregory Bennett.
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. Updated Thu, Jul 3, 1997.