Liquid rocket performance computer model with distributed energy release Interim final report, 15 Aug. 1969 - 15 Aug. 1970 [PDF]
Liquid propellant rocket engine performance computer program with distributed energy ...
Campell, D. T. +2 more
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Operating manual for coaxial injection combustion model [PDF]
An operating manual for the coaxial injection combustion model (CICM) is presented as the final report for an eleven month effort designed to provide improvement, to verify, and to document the comprehensive computer program for analyzing the performance
Chadwick, W. D. +2 more
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A molecular-line study of the interstellar bullet engine IRAS 05506+2414
, 2017 We present interferometric and single-dish molecular line observations of the interstellar bullet-outflow source IRAS 05506+2414, whose wide-angle bullet spray is similar to the Orion BN/KL explosive outflow and likely arises from an entirely different ...
Claussen, Mark +5 more
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Study of thermal protection requirements for a lifting body entry vehicle suitable for near-earth missions Final report [PDF]
Reentry and abort trajectory analyses, and thermal protection requirements for lifting body entry ...
Brunner, M. J. +4 more
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Ceramic thermal-barrier coatings for cooled turbines [PDF]
Coating systems consisting of a plasma sprayed layer of zirconia stabilized with either yttria, magnesia or calcia over a thin alloy bond coat have been developed, their potential was analyzed and their durability and benefits evaluated in a turbojet ...
Liebert, C. H., Stepka, F. S.
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High performance N2O4/amine elements: Data dump covering. Task 1: Literature review [PDF]
The phenomenon of reactive stream separation (RSS) in the N2O4/amine earth-storable propellant combinations is reviewed. Early theoretical models of RSS are presented, as are experimental combustion data under simulated rocket conditions.
Hines, W. S., Nurick, W. H.
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Advanced liner-cooling techniques for gas turbine combustors [PDF]
Component research for advanced small gas turbine engines is currently underway at the NASA Lewis Research Center. As part of this program, a basic reverse-flow combustor geometry was being maintained while different advanced liner wall cooling ...
Norgren, C. T., Riddlebaugh, S. M.
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Mechanical Properties of Cold Gas-Dynamic Spray Nickel [PDF]
, 2000 Decker ,Merlin K. +2 more
openaire +2 more sources
Thermodynamic performance testing of the orbiter flash evaporator system [PDF]
System level testing of the space shuttle orbiter's development flash evaporator system (FES) was performed in a thermal vacuum chamber capable of simulating ambient ascent, orbital, and entry temperature and pressure profiles.
Frahm, J. P. +2 more
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