Hydrazine has been used as an energy source in many applications to fuel in-flight main engine starting. In a current application, an existing hydrazine engine start system (ESS) design was adapted to meet new fuel control requirements. This paper presents a brief system description, historical context and the motivating factors for the hydrazine controls changes, and three case studies of controls design and analysis from the ESS program.
Hydrazine Engine Start System Air Start Performance and Controls Sizing
Sae Technical Papers
Aerospace Technology Conference and Exposition ; 1992
1992-10-01
Conference paper
English
Hydrazine engine start system air start performance and controls sizing
Tema Archive | 1992
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