'Orbit configuration' diaporamas de présentation

THEMIS IDPU FSW V4 Introduction Part III Operations Monday, October 20, 2014

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R. Wang ISS QA

ISSP On-Orbit QA To share with QLF the ISS approach to the On-Orbit Quality Assurance process and the current status NASA QLF 9-25-2002. R. Wang ISS QA. ISSP On-Orbit QA.

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Structural Goals

Structural Goals. The following structural stiffness and strength goals for the launch configuration are recommended for OCE2 and encompass a generic spacecraft and launch vehicle Fundamental Frequency for launch > 35 Hz Based on frequency guidelines associated with component mass of 301 Kg

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