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181   $ctxt$2rdacontent
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200 10$aGas-injection-start and shutdown characteristics of a 2- to 15-kilowatt Brayton power system /$fby Dennis A. Cantoni
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dSeptember 1972.
215   $a1 online resource (17 pages) $cillustrations
225 1 $aNASA/TN ;$vD-6938
300   $a"September 1972."
320   $aIncludes bibliographical references (page 17).
606   $aAerospace vehicles$2nasat
606   $aGas injection$2nasat
606   $aSpace vehicles$xAuxiliary power supply
606   $aSpace vehicles$xAuxiliary power supply$2fast
615  7$aAerospace vehicles.
615  7$aGas injection.
615  0$aSpace vehicles$xAuxiliary power supply.
615  7$aSpace vehicles$xAuxiliary power supply.
700   $aCantoni$b Dennis A.$01401218
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLewis Research Center.
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912   $a9910716558503321
996   $aGas-injection-start and shutdown characteristics of a 2- to 15-kilowatt Brayton power system$93469617
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