Space Shuttle Orbiter Auxiliary Power Unit

820838

2/1/1982

Authors
Abstract
Content
The Space Shuttle Orbiter auxiliary power units (APUs) provide hydraulic power for the Orbiter vehicle control surfaces (rudder/speed brake, body flap, and elevon actuation systems), main engine gimbaling during ascent, landing gear deployment and steering and braking during landing. Operation occurs during launch/ascent, in-space exercise, reentry/descent, and landing/rollout.
Operational effectiveness of the APU is predicated on reliable, failure-free operation during each flight, mission life (reusability) and serviceability between flights (turnaround). Along with the accumulating flight data base, the status and results of efforts to achieve these long-run objectives is presented.
Meta TagsDetails
DOI
https://doi.org/10.4271/820838
Citation
McKenna, R., Wicklund, L., Baughman, J., and Weary, D., "Space Shuttle Orbiter Auxiliary Power Unit," Intersociety Conference on Environmental Systems, San Diego, California, United States, July 19, 1982, https://doi.org/10.4271/820838.
Additional Details
Publisher
Published
2/1/1982
Product Code
820838
Content Type
Technical Paper
Language
English