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Packaging Factors for Extra Vehicular Activity (EVA) Toolboxes Based on Existing ISS and STS Toolboxes
Technical Paper
2002-01-2367
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
Volume and weight will drive selection of toolbox designs for future space missions. A packaging factor to estimate the volume and weight and tool board area of future toolboxes is needed. The purpose of this study is to determine volume, weight, and area packaging factors for use in sizing trade studies of future EVA toolboxes. Packaging factors calculated here are based on operational systems, e.g. the EVA Tool Stowage Device (ETSD) 1 & 2, Airlock EVA Tool Stowage Device 1 (A/L ETSD 1), Airlock EVA Tool Stowage Device 2 (A/L ETSD 2), Tool Stowage Assembly (TSA), lightweight Tool Stowage Assembly (LWTSA), and Hubble Space Telescope (HST) toolbox.
Authors
Citation
Bahnsen, A., Marak, R., and Rouen, M., "Packaging Factors for Extra Vehicular Activity (EVA) Toolboxes Based on Existing ISS and STS Toolboxes," SAE Technical Paper 2002-01-2367, 2002, https://doi.org/10.4271/2002-01-2367.Also In
References
- Packaging Factors for Portable Life Support Subsystems Based on Apollo and Shuttle Systems Thomas Gretchen A. 23 rd International Conference on Environmental Systems Colorado Springs, Colorado July 12-15 1993
- Space Suit Life Support System Packaging Factors Abramov I.P. Sharipov R.K. Skoog A. I Herber Nikolaus 24 th International Conference on Environmental Systems Friedrichshafen, Germany June 23-23 1994