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Design and use of a servo-controlled high pressure window bomb in spectroscopic studies of solid propellant combustionThe feasibility of using a high pressure window bomb as a laboratory scale model of actual motor conditions. The design and operation of a modified high pressure window bomb is discussed. An optical servocontrol mechanism has been designed to hold the burning surface of a propellant strand at a fixed position within the bomb chamber. This mechanism permits the recording of visible and infrared emission spectra from various propellants. Preliminary visible emission spectra of a nonmetalized and metalized propellant are compared with spectra recorded using the modified bomb.
Document ID
19810007759
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Goetz, F.
(Dayton Univ. OH, United States)
Mann, D. M.
(AFRPL)
Date Acquired
August 11, 2013
Publication Date
November 1, 1980
Publication Information
Publication: NASA. Langley Research Center The 17th JANNAF Combust. Meeting, Vol. 1
Subject Category
Propellants And Fuels
Accession Number
81N16275
Funding Number(s)
CONTRACT_GRANT: F04611-77-C-0042
Distribution Limits
Public
Copyright
Other

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