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Design Study for A Low-Cost LH2 TurbopumpA preliminary design study, focusing on potential component selections and design for manufacturing and assembly (DFMAR1) analysis, is presented in this study. The investigation focused on a nominal cost liquid hydrogen turbopump suitable for a private launch class vehicle. Utilizing a "turbocharger-like" design philosophy, preliminary feasibility studies of the basic pump design class, the rotordynamic design class, and the turbine design class were conducted with associated DFMA evaluations. Reasonable cost levels and sensible levels of product assurance have been established.
Document ID
20010021726
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Japikse, David
(Concepts ETI, Inc. White River Jct, VT United States)
Baines, Nicholas
(Concepts ETI, Inc. White River Jct, VT United States)
Platt, Michael J.
(Concepts ETI, Inc. White River Jct, VT United States)
Date Acquired
August 20, 2013
Publication Date
November 1, 2000
Publication Information
Publication: JANNAF 1st Modeling and Simulation Subcommittee Meeting
Subject Category
Mechanical Engineering
Meeting Information
Meeting: Modeling and Simulation Subcommittee
Location: Monterey, CA
Country: United States
Start Date: November 13, 2000
End Date: November 17, 2000
Sponsors: NASA Headquarters, Department of the Navy, Department of the Air Force, Department of the Army
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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