Ignition characterization of LOX/hydrocarbon propellants
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Ignition characterization of LOX/hydrocarbon propellants final report

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Published by The Center, National Technical Information Service, distributor in Houston, Tex, [Springfield, Va .
Written in English

Subjects:

  • Liquid oxygen.,
  • Space vehicles -- Propulsion systems.

Book details:

Edition Notes

Statementprepared for NASA-Lyndon B. Johnson Space Center ; B.R. Lawver, D.C. Rousar, K.Y. Wong.
SeriesNASA contractor report -- NASA CR-171884.
ContributionsRousar, D. C., Wong, K. Y., Lyndon B. Johnson Space Center.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL15386266M

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Ignition characterization was accomplished through the analysis, design, fabrication and testing of a spark initiated torch igniter and prototype lbF thruster/igniter assembly. The igniter was tested over a chamber pressure range of 74 to psia and mixture ratio range of to Ignition characterization of LOX/hydrocarbon propellants final summary report (SuDoc NAS ) [B. R. Lawver] on *FREE* shipping on qualifying offers. Get this from a library! Ignition characterization of LOX/hydrocarbon propellants: final report. [B R Lawver; D C Rousar; K Y Wong; Lyndon B. Johnson Space Center.]. Get this from a library! Ignition characterization of LOX/hydrocarbon propellants: final summary report. [B R Lawver; Lyndon B. Johnson Space Center.].

Ignition characterization of LOX/hydrocarbon propellants eBook: National Aeronautics and Space Administration NASA: : Kindle StoreAuthor: National Aeronautics and Space Administration NASA. The features which make the LOX/hydrocarbon propellants attractive are their good performance combined with high bulk density (relative to hydrogen), low cost, and ease of handling. L0X/RP-1, in particular, has been used with success on a number of operational engines (F-l, Author: R.J. LaBotz, R.L. Ewen. What mineral is used in rocket propellants? Unanswered Questions. What is the particular type of processor model and operating system on which a computer is based called. Download Citation | Ignition Thresholds and Combustion Efficiencies of Non-Cryogenic ICF Targets | We present a theoretical study of ignition thresholds and combustion efficiencies of .

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