The Development of Fans for the International Space Station

972382

07/01/1997

Event
International Conference On Environmental Systems
Authors Abstract
Content
The use of rapid prototyping in the development of five fans for the International Space Station is reviewed, showing how the design cycle has been reduced by more than 75% through the use of rapid prototype hardware test articles. A case study shows how rapid prototyping was used to produce a fan's two housings and how four separate impellers were designed, fabricated and tested in a five week period. Both aerodynamic and acoustic performance of the rapid prototype hardware were validated by flight-version metal assemblies. Using the improved development process where only two parts are changed to existing space-qualified fans shows that a broad range in flow and ΔP capability exists for designs targeted to specific operating points.
Meta TagsDetails
DOI
https://doi.org/10.4271/972382
Pages
9
Citation
Converse, D., "The Development of Fans for the International Space Station," SAE Technical Paper 972382, 1997, https://doi.org/10.4271/972382.
Additional Details
Publisher
Published
Jul 1, 1997
Product Code
972382
Content Type
Technical Paper
Language
English