Advanced Inflatable Airlock System for EVA

2002-01-2314

07/15/2002

Authors Abstract
Content
The Advanced Inflatable Airlock (AIA) System is currently being developed for the 2nd Generation Reusable Launch Vehicle (RLV). The objective of the AIA System is to greatly reduce the cost associated with performing extravehicular activity (EVA) from the RLV by reducing launch weight and volume from previous hard airlock systems such as the Space Shuttle and Space Station airlocks. The AIA System builds upon previous technology from the TransHab inflatable structures project, from Space Shuttle and Space Station Airlock systems, and from terrestrial flexible structures projects. The AIA system design is required to be versatile and capable of modification to fit any platform or vehicle needing EVA capability. This paper discusses the AIA conceptual design and key features that will help meet the 2nd Generation RLV program goals of reduced cost and program risk.
Meta TagsDetails
DOI
https://doi.org/10.4271/2002-01-2314
Pages
7
Citation
Campbell, A., Barido, R., Knudsen, J., MacKnight, A. et al., "Advanced Inflatable Airlock System for EVA," SAE Technical Paper 2002-01-2314, 2002, https://doi.org/10.4271/2002-01-2314.
Additional Details
Publisher
Published
Jul 15, 2002
Product Code
2002-01-2314
Content Type
Technical Paper
Language
English