Power switching trims digital system weight, cost.
Series power switch for orientation and position computer of small lunar-orbit spacecraft designed to reduce weight and cost
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Series power switch for orientation and position computer of small lunar-orbit spacecraft designed to reduce weight and cost
Radiation, molecular orientation, crystallinity and molecular weight influences on thermoconductivity of high polymers
Digital computer program for analysis and weight optimization of thermoelectric generators for space applications
Combinatorial formula for calculating coding vector sums - weight distribution moments of binary code - communication system
Viscoelastic properties of polyvinyl acetates - mechanical loss and molecular weight distribution
Stiffener eccentricity and location influence on minimum weight design aspects of stiffened cylinders under compression
Weight-area tradeoff evaluation of radiator used in SNAP-8
Gas chromatograph apparatus for preparing ultrahigh molecular weight polyethylene terephthalate from solid state commercial grade material
Effects of weight limitations on optimal motion of variable mass body with limited velocity jet
Molecular weight sensitivity of thermoconductivity of polydimethylsiloxane and polyethyleneglycol
Lagrange multiplier matrix in minimum weight and fully stressed optimum structural design techniques
Axially loaded cylindrical structures analyzed for optimum weight construction consistent with cost constraint, emphasizing beryllium-aluminum alloys
Ultrahigh molecular weight poly/ethylene terephthalate/ synthesized, studying catalyst, particle size, reaction temperature and time and carrier gas flow rate
Molecular weight and amino acid composition of chromatium ferredoxin
Weight loss of astronauts during space flight due to blood pooling
Various details of design or arrangement of the parts of airplane structures are shown and discussed, the use of these devices having resulted in the production of structures of adequate strength, yet of a weight less than one-half of the usual construction.
In the foregoing remarks I have made an attempt to touch on some of the structural problems met with in cantilever wings, and dealt rather fully with a certain type of single-spar construction. The experimental test wing was a first attempt to demonstrate the principles of this departure from orthodox methods. The result was a wing both torsionally stiff and of light weight - lighter than a corresponding biplane construction.
Artificial RNAs (aRNAs) containing novel sequence segments embedded in a deletion mutant of Vibrio proteolyticus 5S rRNA have previously been shown to be expressed from a plasmid borne growth rate regulated promoter in E. coli. These aRNAs accumulate to high levels and their detection is a promising tool for studies in molecular microbial ecology and in environmental monitoring. Herein a new construct is described which illustrates the versatility of detection that is possible with aRNAs. This 3xPen aRNA construct carries a 72 nucleotide insert with three copies of a unique 17 base probe target sequence. This aRNA is 160 nucleotides in length and again accumulates to high levels in the E. coli cytoplasm without incorporating into ribosomes. The 3xPen aRNA illustrates two improvements in detection. First, by appropriate selection of insert size, we obtained an aRNA which provides a unique and hence, easily quantifiable peak, on a high resolution gel profile of low molecular weight RNAs. Second, the existence of multiple probe targets results in a nearly commensurate increase in signal when detection is by hybridization. These aRNAs are naturally amplified and carry sequence segments that are not found in known rRNA sequences. It thus may be possible to detect them directly. An experimental step involving RT-PCR or PCR amplification of the gene could therefore be avoided.