Mission Design - First Flight
Section 4.1.
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Table of Spacecraft and Fuel Masses

The spacecraft mass, specific impulse (ISP), and fuel requirements listed below match up with the reference mission timeline of burns and maneuvers.

LTV CM Dry Weight        4,000 lbs  (1,814 kg)
LTV SM Dry Weight        3,000 lbs  (1,361 kg)
LTV TLI Fuel            50,843 lbs (23,062 kg)
LTV LUNO Insert Fuel       724 lbs    (328 kg)
LTV LUNO Circ Fuel         139 lbs     (63 kg)
LTV Plane Change Fuel      218 lbs     (99 kg)
LTV TEI Fuel             4,258 lbs  (1,931 kg)
LTV LEOI Fuel            8,968 lbs  (4,068 kg)
ISP LTV                    460 sec

Hab Weight              15,000 lbs  (6,804 kg)
Airlock Weight             600 lbs    (272 kg)
Desc Dry Weight            900 lbs    (408 kg)
ISP Desc                   460 sec

Asc Dry Weight           1,600 lbs    (726 kg)
Asc Fuel                 1,730 lbs    (785 kg)
ISP Asc                    260 sec

The reference mission timeline is in section 4.1.1 of the Artemis Data Book.

Mission Design - First Flight

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