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Super Integrated Power Unit (SIPU) for the F-16 Engine Start System Sundstrand Aviation, Div. of Sundstrand Corporation, Rockford, IL

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Smith, W. Glen, author.
Conference Name:
Aerospace Congress & Exposition (1982-10-25 : Anaheim, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1982
Summary:
The F-16 main engine inflight restart capability would be greatly enhanced by utilizing a Super Integrated Power Unit (SIPU). Because the available starter power remains constant at all altitudes, the engine can be motored at relatively high rotative speeds, providing for rapid acceleration to a self sustaining condition after relight. This reduced start time plus a multiple start capability, reduces altitude loss and increases safety during combat. The SIPU concept expands the airstart window and allows the pilot to assume a "best range" flight attitude which maximizes both time and range by up to 35% in the event the engine is not able to start
Notes:
Vendor supplied data
Publisher Number:
821462
Access Restriction:
Restricted for use by site license

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