NDLI: Passive suppression of pogo on the space shuttle

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Passive suppression of pogo on the space shuttle

Content Provider	NASA Technical Reports Server (NTRS)
Author	Rubin, S. Lock, M. H.
Copyright Year	1974
Description	A qualitative assessment of the tendency for pogo instability of the shuttle vehicle in the absence of suppression devices, and the effectiveness of two passive suppressors (the compliant accumulator and the resistive accumulator) in counteracting any tendency toward instability is provided. In addition, the relative effectiveness of three suppressor locations (the low pressure pump (LWOP) inlet and discharge and the high pressure pump (HPOP) inlet) is also evaluated. The primary conclusion of the study is that effective pogo suppression, with passive devices, can be accomplished at the HPOP inlet location but not at the LPOP locations. Other conclusions are drawn regarding the relative effectiveness of the two accumulator types and with respect to tentative accumulator design requirements. Finally, a number of recommendations are made regarding future studies.
File Size	1277482
Page Count	81
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19740021169
Archival Resource Key	ark:/13960/t2t48g53p
Language	English
Publisher Date	1974-04-29
Access Restriction	Open
Subject Keyword	Space Vehicles Pogo Effects Spacecraft Stability Propulsion System Configurations Longitudinal Stability Space Shuttles Accumulators Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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