a study of Self-Contained Starting Systems for Turbojet and Turboprop Engines

600011

01/01/1960

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
SUBSTANTIAL POWER is necessary to start the modern jet engine. Thus, starting equipment has become a major concern of air transport operators. This paper discusses the equipment used with self-contained starting systems.
The authors discuss and evaluate a variety of self-contained systems: combustor, fuel-air combustion, cartridge, liquid propellant, hydraulic supported by auxiliary power units, and electric supported by APU. Possible future systems are: self-breathing systems, oxygen combustors, and liquid-oxygen-water-fuel combustors.
It is emphasized that the choice of a starting system for a particular aircraft will depend on aircraft characteristics and the aircraft's intended use.*
Meta TagsDetails
DOI
https://doi.org/10.4271/600011
Pages
14
Citation
Schmider, H., and Ferguson, J., "a study of Self-Contained Starting Systems for Turbojet and Turboprop Engines," SAE Technical Paper 600011, 1960, https://doi.org/10.4271/600011.
Additional Details
Publisher
Published
Jan 1, 1960
Product Code
600011
Content Type
Technical Paper
Language
English