Super Integrated Power Unit (SIPU) for the F-16 Engine Start System

821462

02/01/1982

Authors
Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/821462
Pages
12
Citation
Smith, W., and Fandel, R., "Super Integrated Power Unit (SIPU) for the F-16 Engine Start System," SAE Technical Paper 821462, 1982, https://doi.org/10.4271/821462.
Additional Details
Publisher
Published
Feb 1, 1982
Product Code
821462
Content Type
Technical Paper
Language
English