Transient Thermal Simulation of Apollo Spacecraft and ECS Apollo Support Dept., General Electric Company

Format:

Conference/Event

Author/Creator:

Frahm, J. R., author.

Conference Name:

Aeronautic and Space Engineering and Manufacturing Meeting (1967-10-02 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1967

Summary:

An analytical thermal model of the project Apollo Command Module has been developed by the General Electric Company, Apollo Support Dept. for the National Aeronautics and Space Administration, Manned Spacecraft Center. This model simulates the entire spacecraft structure and the four closed fluid loops of the Environmental Control System.The configuration of the model is discussed as well as the correlation of this type model with test data. Also covered are the environmental data used in conjunction with the model for mission analysis. Typical results of the mission analyses are discussed in more detail

Notes:

Vendor supplied data

Publisher Number:

670837

Access Restriction:

Restricted for use by site license