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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Aerodynamic characteristics of aircraft configuration for low level supersonic attack tested in transonic wind tunnel
Simulated rocket jet exhaust effect on stability and control of research aircraft configuration
Factors affecting static, longitudinal, and directional stability characteristics of supersonic aircraft configurations
Reentry vehicle configuration from manned Mars missions, using aerobraking
Nuclear-electric spacecraft configurations for Jupiter mission discussing radiation shielding, heat rejection radiator, spacecraft structure, etc
Engine nacelle orientation effect on aerodynamic characteristics of arrow wing body configuration
Effects on Scout launch vehicle structure due to unconventional vehicle-spacecraft configurations
Hypersonic aerodynamic characteristics of aircraft configurations with canard controls
Effects of applying thrust along with optimum aerodynamic control surface defections on incipient and developed spin-recovery characteristics of four aircraft configurations
Aerodynamic characteristics of aircraft configuration having tail surfaces outboard of wing tips at supersonic speeds - wind tunnel stability test
Supersonic study of configuration geometry effects on pressure-coefficient and section normal-force- coefficient distributions for two-stage launch vehicle
Longitudinal aerodynamic characteristics of tension shell entry configuration at Mach 20
Subsonic and supersonic aerodynamic characteristics of aircraft configuration using double pivot variable sweep wings
Airplane configuration effect on shape and magnitude of sonic boom pressure signature, noting theoretical and empirical methods
Matrix-Holzer analyses for predicting free vibration modes of clustered launch vehicle configurations including Titan IIIC and uncoupled Saturn I cases
Nuclear electric spacecraft configurations effects on mass of spacecraft radiation shield, heat rejection radiators, booster adapter, and aerodynamic shroud subsystems
Pressure tunnel investigation of supersonic store interference in vicinity of 22 deg swept wing fuselage configuration at mach numbers 1.61 and 2.01
Contractor data package for Voyager spacecraft configuration management