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Diffuser investigation for advanced multi-megawatt MPD engine developmentSteady-state testing of advanced, multimegawatt MPD engines requires vacuum facilities with pumping speeds which are not presently available. Gas dynamic diffusers have been proposed as a possible solution to this problem. An analytical investigation into the feasibility of using a diffuser for pumping the MPD engine exhaust is presented here. This analysis uses a detailed equation of state based on the partition function for the high temperature argon exhaust. On the basis of the electron-ion momentum exchange collision frequency in the exhaust plasma, it was concluded that the diffuser gas dynamics could be modeled to a first approximation with ordinary continuum equations. Calculations of the stagnation pressure in the diffuser, downstream of a strong normal shock, yielded pressures on the order of 10 torr suggesting that the diffuser is feasible for pumping the MPD engine exhaust.
Document ID
19860057903
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brophy, J. R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
King, D. Q.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 86-1436
Report Number: AIAA PAPER 86-1436
Accession Number
86A42641
Distribution Limits
Public
Copyright
Other

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