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The Crew Control Module for safe crew transportation to and from space. It takes the form of a capsule shape, much like the Apollo Command Module.

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The Resource Module that provides mission power, cooling, and propulsion to Boeing’s envisioned Crew Control Module.

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Delta IV Heavy Launch vehicle capable of transporting Boeing’s envisioned Crew Exploration System elements to low Earth orbit.

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A lunar propulsion system derived from two Delta IV Upper Stages assembled in Low Earth Orbit.

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A robotic cargo vehicle capable of transporting pressurized and non-pressurized cargo to space and back to Earth. It uses the same Resource Module as does the Crew Control Module to supply power, cooling and propulsion.

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An inflatable habitat derived from the Autonomous Cargo Vehicle for use in space, lunar or other planetary surface applications. Its inflatable section is pressurized once at its destination to enhance crew habitability and operations.

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Delta IV vehicle launching the Boeing envisioned Crew Control Module with Crew Escape system and Resource Module to low Earth orbit.

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Crew Exploration Vehicle composed of a Translunar Insertion Stage, a Resource Module and Crew Control Module.

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Assembly base for Lunar Landing Vehicles, Space Telescopes and Interplanetary Transfer Vehicles, assembled in lunar orbit using derivatives of the Autonomous Cargo Vehicle and Crew Habitat.

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Inflatable habitat for an initial lunar surface base, using a derivative Resource Module to land on the lunar surface and providing power and cooling to the Crew.

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Enhanced CEV capable of traveling to Mars or beyond, assembled at the Lunar Space Station and using derivatives of the Crew Control Module, Autonomous Cargo Vehicle and Crew Habitat.

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A Launch Escape System that ensures crew safety during the launch.