Analysis of baseline and Gemini 7 electroencephalogram data with specification of on-line computing requirements
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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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Detailed cost analysis of Advanced Multipurpose Large Launch Vehicle, including cost summary tables
Cost analysis of nonrecurring development testing costs for AMLLV
Detailed cost analysis of recurring elements in multipurpose launch vehicle
Nonrecurring cost analysis for launch vehicles
Cost analysis of nonrecurring development and testing of launch vehicles
Recurring cost analysis for first unit of configuration
Jupiter decametric radio bursts observed by tape recording fringe interferometer
No abstract available
Reusable nuclear shuttle configuration, mass characteristics, stage and INT-21 interfaces, and design criteria and constraints
Personal hygiene protocol for man in spacecraft environment
Quasar internal kinematics and fine structure rapid time variations from radio interferometry
The space shuttle system as it relates to payloads is described. This study provides potential users of the space shuttle with a uniform base of information on the accommodations between the payload and the shuttle. By utilizing this information, preliminary payload planning and design studies can be evaluated and compared against a common set of shuttle/payload accommodations. This information also minimizes the necessity for each payload study to develop information on the shuttle configuration.
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The spectrobolometer used in the studies is discussed, giving attention to instrument design, the method of recording, and the spectral resolution. The atmospheric transmission for each wavelength was determined by making observations over a range of air masses. The precipitable water vapor values were found from the spectrobolograms by measurement of the depths of water vapor bands at 0.935, 1.13, and 1.47 microns. The results of the studies are discussed together with seasonal variations, long term trends, and the nature of the aerosols.
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Preliminary Apollo 14 (Mission H-3) trajectory data for the July 1970 launch window are presented in this document. A general mission profile is presented, and approximate variations of selected mission parameters are indicated. Note that the information in this document is preliminary and will be updated in the Apollo 14 (Mission H-3) operational trajectory documents.