Space Crew Radiation Exposure Analysis System Based on a Commercial Stand-Alone CAD System Boeing Defense and Space Advanced Civil Space Systems Group

Format:

Conference/Event

Author/Creator:

Appleby, Matthew H., author.

Conference Name:

International Conference On Environmental Systems (1992-07-12 : Seattle, Washington, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1992

Summary:

Major improvements have recently been completed in the approach to spacecraft shielding analysis. A Computer-Aided Design (CAD)-based system has been developed for determining the shielding provided to any point within or external to the spacecraft. Shielding analysis is performed using a commercially available stand-alone CAD system and a customized ray-tracing subroutine contained within a standard engineering modeling software package.This improved shielding analysis technique has been used in several vehicle design projects such as a Mars transfer habitat, pressurized lunar rover, and the redesigned Space Station. Results of these analyses are provided to demonstrate the applicability and versatility of the system

Notes:

Vendor supplied data

Publisher Number:

921372

Access Restriction:

Restricted for use by site license