Systems performance/design requirements specification for the CH-46C helicopter digital flight control and landing system
Systems performance/design requirements specifications for CH-46C helicopter digital flight control and landing system
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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
Solid Ne isotopes specific heat at constant pressure and volume, entropy, enthalpy and Gruneisen parameters
Ammonium chloride specific heat measurement near order-disorder transition, comparing results to Ising model behavior
Discrete time digital flight control systems design resulting in closed loop aircraft response characteristics approximation to prescribed flying quality specifications
Specific heat of Apollo 11 breccia and Apollo 12 olivine dolerite at 95-340 K
Experiments with the Data Collection System (DCS) of the Earth Resources Technology Satellites (ERTS) have been developed to stress ERTS applications in the Earth Resources Observation Systems (EROS) Program. Active pursuit of this policy has resulted in the design of eight specific experiments requiring a total of 98 DCS ground-data platforms. Of these eight experiments, six are intended to make use of DCS data as an aid in image interpretation, while two make use of the capability to relay data from remote locations. Preliminary discussions regarding additional experiments indicate a need for at least 150 DCS platforms within the EROS Program for ERTS experimentation. Results from the experiments will be used to assess the DCS suitability for satellites providing on-line, real-time, data relay capability. The rationale of the total DCS network of ground platforms and the relationship of each experiment to that rationale are discussed.