Discover System Effectiveness

Transport delays associated with the NASA Langley flight simulation facility

40 HP electro-mechanical actuator

Hypervelocity launcher for aerothermodynamic experiments

2 kWe Solar Dynamic Ground Test Demonstration Project

Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport

Transport systems research vehicle color display system operations manual

Airbreathing/rocket single-stage-to-orbit design matrix

40 HP electro-mechanical actuator

Characterization and cycle tests of lightweight nickel electrodes

System life and reliability modeling for helicopter transmissions

Semiannual project report submitted to the National Aeronautics and Space Administration, Langley Research Center, Hampton, Va. for research entitled experiments in fault tolerant software reliability