Propellant interaction with the payload control system of dual-spin spacecraft

Significant interaction between the payload control system and the liquid propellant on dual-spin spacecraft is shown to exist for a new class of vehicles with large liquid mass fractions. Experience during the transfer orbit operations of the first two LEASAT synchronous orbit communications satell...

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Bibliographische Detailangaben

Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 1988-07, Vol.11 (4), p.343-351
Hauptverfasser:	SLAFER, LOREN I., CHALLONER, A. DORIAN
Format:	Artikel
Sprache:	eng
Schlagworte:	Communications satellites Experiments Laboratories Payload control
Online-Zugang:	Volltext
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