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
Startsystem mit Hydrazinmotor - Bewertung der Startleistung im Flug und Auslegung der Steuerungselemente
SAE Technical Papers ; 1-14
1992
14 Seiten, 9 Bilder, 1 Tabelle, 4 Quellen
Aufsatz (Konferenz)
Englisch
Hydrazine Engine Start System Air Start Performance and Controls Sizing
SAE Technical Papers | 1992
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