| Document Date: 2012-01-11 12:39:39
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City San Francisco / / / IndustryTerm assumed technology level / present technologies / technology effort / assumed engine technology / Gas turbine engines / gas turbine components / technology factors / updated technology assumptions / gas turbine analyses / thermodynamic models using technology / assumed aerodynamics technology / technology assumptions / propulsion systems / engine technology / equivalent turbine technology / minimum weight solution / aggressive technology push / / Organization U. S. Government / National Aeronautics and Space Administration / NASA Large Civil Tiltrotor / LCTR2 mission / MRP OEI / / Person ISA KCAS / Christopher A. Snyder / C. W. Acree / Jr. / / Position candidate for future studies / Aerospace Engineer / representative / Engineer / / ProgrammingLanguage RC / / ProvinceOrState California / / Technology SOA / equivalent turbine technology / assumed aerodynamics technology / assumed engine technology / engine technology / VSPT technology / Simulation / representative steady-state / thermodynamic models using technology / 6.0 Key Technology / /
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Influence of Alternative Engine Concepts on LCTR2 Sizing and Mission Profile C. W. Acree, Jr. Aerospace Engineer NASA Ames Research Center [removed] Christopher A. Snyder