| A/C Ai APU BIT BITE CAPSS CIL c/o CoFR DDT&E DMES ECLSS EMA ET FMEA GH2 GHe GLOW GN2 GNP GO2 GPSS GSE GUCP H2 HCF HCFC HGDS Hp HRST I/F Isp LCC LCF LDT LH2 LHe LO2 LOX LRU MCC MMH MPS MTBF MTTR N2O4 NDE NH3 nm O2 OMRS OMS OPF OSAMS PA PCA PDR PR PRACA PVT QFD R&D RBCC RCS RLV RM&S ROM RP-1 SCAN SPST SRB SSME SSTO TRL TSM TVC VHM |
Air Conditioning Availability, Inherent Auxiliary Power Unit Built in Test Built in Test Equipment Computer Aided Planning and Scheduling System Critical Items List Checkout Certificate of Flight Readiness Design, Development, Test and Engineering Dimethylethoxysilane Environmental Control and Life Support System Electromechanical Actuator External Tank Failure Mode Effects Analysis Gaseous Hydrogen Gaseous Helium Gross Lift Off Weight Gaseous Nitrogen Gross National Product Gaseous Oxygen Ground Processing Scheduling System Ground Support Equipment Ground Umbilical Carrier Plate Hydrogen High Cycle Fatigue Hydrochlorofluorocarbons Hazardous Gas Detection System Horsepower Highly Reusable Space Transportation Interface Specific Impulse Life Cycle Cost Low Cycle Fatigue Logistics Down Time Liquid Hydrogen Liquid Helium Liquid Oxygen Liquid Oxygen Line Replaceable Unit Main Combustion Chamber Monomethylhydrazine Main Propulsion System Mean Time Between Failure Mean Time to Repair Nitrogen Tetroxide Non-Destructive Test Ammonia Nautical mile Oxygen Operations Maintenance Requirement Specification Orbital Maneuvering System Orbiter Processing Facility Operation Simulation and Analysis Modeling System Program Acquisition Precision Cleaning Agent Preliminary Design Review Problem Report Problem Reporting and Corrective Action Pressure, Volume, Temperature Quality Function Deployment Research and Development Rocket Based Combined Cycle Reaction Control System Reusable Launch Vehicle Reliability, Maintainability, and Supportability Rough Order of Magnitude Rocket Propellant, Kerosene Shuttle Connector Analysis Network Space Propulsion Synergy Team Solid Rocket Booster Space Shuttle Main Engine Single Stage to Orbit Technology Readiness Level Tail Service Mast Thrust Vector Control Vehicle Health Management |
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Edgar Zapata, NASA Kennedy Space Center
Shuttle Process Engineering Directorate, Fluid Systems Division