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Performance of a short modular turbojet combustor segment using ASTM-A1 fuel [NASA TN D-6167]

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Material type: Text

TextLanguage: English Publication details: Washington, D. C. NASA February 1971Description: 32pSubject(s):

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NASA technical note

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference		Not for loan		TR013034

Total holds: 0

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Previous	Experimental performance and combustion stabilty of a full scale duct burner for a supersonic turbofan engine [NASA TN D-6163]tburner for a supersonic turbofan engine [NASA TN D-6161]	An study of shaft face sear self acting lift augmentatuio [NASA TN D-6164]	Preliminary friction and wear studies ogf cobalt rehenium solid solution alloy in air and in vaccum [NASA TN D-6165]	Performance of a short modular turbojet combustor segment using ASTM-A1 fuel [NASA TN D-6167]	The gas phase in porous fuel cell electrodes [NASA TN D-6168]	Neutronic design for a lithium cooled reactor for space applications [NASA TN D-6169]	A study of some transitions matrix assunptions in circumlunar navigation theory [NASA TN D-1812]	Next

NASA technical note

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