Anomalous substrate specificities among the algal peroxidases
Anomalous substrate oxidizing specificities among red brown and green algal peroxidases and land plants
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Anomalous substrate oxidizing specificities among red brown and green algal peroxidases and land plants
Low specific impulse hollow cathode mercury thrustor for deep space electric propulsion, using SERT 2 configuration
Apollo 11 sample specific heats at 90-350 K, using adiabatic calorimeter
Specific heat of amorphous polymethyl methacrylate and polystyrene by pulse method below 4 K, comparing Debye and acoustic values
The NASA Flight Research Center is reviewing the applicability of flying qualities experience to the shuttle mission for the purpose of preparing a shuttle flying qualities specification. This paper is a progress report on this review; the results presented are, of course, preliminary.
Systems performance/design requirements specifications for CH-46C helicopter digital flight control and landing system
Engineering specifications of signature data processing system for automatic extraction of spectral information from multispectral band scanners - Vol. 3
Isotope effects in specific heat of solid neon
Equipment specifications for Lunar Sounder Antenna Assembly
Effects of specific speed on experimental performance of radial inflow turbine
Calculated estimates of gas core nuclear rocket engine weights for specific impulses ranging from 3000 to 7000 seconds and for engine thrusts ranging from 4400 to 440,000 newtons
Major and critical component specifications for construction of simulator cruise scene visual attachment for manned spacecraft or aircraft flight simulation
Requirement specifications for environmental laboratory test chamber complex design, fabrication, and testing
System configuration and executive requirements specifications for reusable shuttle and space station/base
Specifications for cleaning, fusion welding, and postheating tantalum and niobium alloys
Space communication system specification and performance criteria
Nozzle and cavity wall cooling limitations on specific impusle of gas-core nuclear rocket engine
Executive routine primitives and process control for spaceborne computer functional design specification - Vol. 3