CEV Design

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My design is very similar to the Orion, yet not quite the same. The shape of the service module is spherical, since it is the most efficient 3D shape, while the command module has a cone-like form. This CEV is propelled by a single OMS (orbital maneuvering system) engine on the end of the service module. The booster will use a methane/oxygen fuel rather than the hydrazine/nitrogen tetroxide fuel used on Apollo because it has a greater specific impulse, which means it burns longer for the same amount. Four RCS (reaction control system) thrusters located on the command module above the engine can change the orientation of the craft in space. They allow the CEV to make pitch, roll, and yaw rotational maneuvers as well as translation maneuvers along the X, Y, and Z axes. The guidance, navigation, and control system is all about the destination, current location, and path of the CEV. These devices detect the vehicle’s motion and informs the GNC what is happening. Inertial measurement units (IMUs) contain gyros to measure and provide inertial attitude and velocity data to the G...

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