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Space Shuttle Orbiter Auxiliary Power Unit Sundstrand Energy Systems, Rockford, IL

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
McKenna, R., author.
Conference Name:
Intersociety Conference on Environmental Systems (1982-07-19 : San Diego, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1982
Summary:
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
Notes:
Vendor supplied data
Publisher Number:
820838
Access Restriction:
Restricted for use by site license

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