Space Shuttle Orbiter Auxiliary Power Unit

820838

02/01/1982

Event
Intersociety Conference on Environmental Systems
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
Pages
12
Citation
McKenna, R., Wicklund, L., Baughman, J., and Weary, D., "Space Shuttle Orbiter Auxiliary Power Unit," SAE Technical Paper 820838, 1982, https://doi.org/10.4271/820838.
Additional Details
Publisher
Published
Feb 1, 1982
Product Code
820838
Content Type
Technical Paper
Language
English