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Environmental Control of Apollo Applications Program Orbital Assembly
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English
Abstract
The approach used to integrate the thermal and life support systems of several large spacecraft is presented. These spacecraft will be assembled in earth orbit to make up the Apollo Applications Program (AAP) Orbital Assembly (OA). Due to the size of the spacecraft and the complexity of the systems involved, it was necessary to analyze the thermal and life support systems by defining appropriate interfaces and integrating the results into overall system math models.
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Authors
Citation
Cody, J., "Environmental Control of Apollo Applications Program Orbital Assembly," SAE Technical Paper 690622, 1969, https://doi.org/10.4271/690622.Also In
References
- Hastings, L. J. Patterson W. C. Ward, W. D. “Thermal Control of the Orbital Workshop.” Paper 690624 presented at SAE National Aeronautics and Space Meeting, Los Angeles October 1969
- Calhoune, L. D. “Airlock Module Environmental Control and Life Support Systems.” Paper 690623 presented at SAE National Aeronautics and Space Meeting, Los Angeles October 1969
- Gillerman, J. B. “A Regenerative Carbon Dioxide Removal System for the AAP Cluster.” Paper 690626 presented at SAE National Aeronautics and Space Meeting, Los Angeles October 1969