Snatch force during lines-first parachute deployments
Snatch force during lines-first deployment of aerodynamic decelerator, including effects of canopy skirt acceleration and suspension wave propagation characteristics
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Snatch force during lines-first deployment of aerodynamic decelerator, including effects of canopy skirt acceleration and suspension wave propagation characteristics
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For abstract, see N74-19673.
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(Previously cited in issue 01, p. 17, Accession no. A82-10418)
Previously cited in issue 24, p. 3752, Accession no. A82-48043
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New arrangement provides nearly uniform distribution of load among vent lines and points of attachment of vent lines to vent band. New method eliminates large stack height between first and last lines and, just as important, maintains constant stack height between any two adjacent vent lines around entire vent. Distributes loads at vent band more nearly evenly among lines. Adverse concentrations of loads in vent band reduced.
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Systematic variations in the 13C contents of individual extractable n-alkanes (C16-C29) can be modelled quantitatively and interpreted as indicating contributions from at least five distinct sources. These appear to be cyanobacterial (C16-C18, delta 13C = -37% vs PDB), phytoplanktonic (C16-C23, delta = -32%), chemoautotrophic bacterial (C20-C29, delta = -38%), phytoplanktonic or heterotrophic bacterial (C20-C29, delta = -30%), and vascular plants (C23-C29, delta = -29%). Hydrous pyrolysis of related kerogens yields large quantities of additional n-alkanes with different and much more uniform delta values. The latter materials are apparently derived from the thermolysis of aliphatic biopolymers whose presence in the Green River Oil Shale has been recognized visually.
Canopy Model IV was tested in four different configuration series. Shroud lines were used in the first three series of tests; none were used in the fourth series. Other variables were Mach number (1.77, 2.17, 2.76), dynamic pressure (290, 250, 155 lb per sq ft), camera speed, and attitude.
A forced oscillation test of the Orion Crew Module (CM) was conducted in the Langley 20-Foot Vertical Spin Tunnel. The objective of the test was to quantify the rate damping characteristics of the CM-drogue chute system. Numerous configurations were tested to measure the influence of the chutes on the CM dynamic aerodynamics and, conversely, the influence of the CM on drogue performance. Results show that the CM-drogue system is well-damped at all combinations of frequency, amplitude, and Strouhal number. The wake of the CM significantly reduces the drogue chute riser line force, and the drogues have little upstream influence on the CM aerodynamics. These results are being used to improve simulation model fidelity of CM flight with drogues deployed, which has been identified by the project as key to a successful Orion Critical Design Review.