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Deployment

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• Parachutes -- Deployment
• Water patrol -- Deployment

• Experimental investigation of packaging and deployment characteristics of an inflatable toroidal-space-station configuration (National Aeronautics and Space Administration ;, 1965), by Clarence O. Keffer and Langley Research Center (page images at HathiTrust)
• Flight test of a 30-foot nominal diameter disk-gap-band parachute deployed at a Mach number of 1.56 and a dynamic pressure of 11.4 pounds per square foot (National Aeronautics and Space Administration ;, 1967), by Clinton V. Eckstrom, John S. Preisser, and Langley Research Center (page images at HathiTrust)

• NASA TN D-5911 (National Aeronautics and Space Administration ;, 1970), by Harry L. Morgan, Charles F. Bradshaw, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Techniques for selection and analysis of parachute deployment systems (National Aeronautics and Space Administration ;, 1970), by Earle K. Huckins and Langley Research Center (page images at HathiTrust)
• Flight test of a 15-foot-diameter (4.6-meter) 120 ̊conical spacecraft simulating parachute deployment in a Mars atmosphere (National Aeronautics and Space Administration ;, 1967), by Wayne L. Darnell, Reginald R. Lundstrom, Allen B. Henning, and Langley Research Center (page images at HathiTrust)
• NASA TN D-4123 (National Aeronautics and Space Administration ;, 1967), by Richard L. Barton and United States National Aeronautics and Space Administration (page images at HathiTrust)
• WInd-tunnel investigation of the opening characteristics, drag, and stability of several hemispherical parachutes (National Advisory Committee for Aeronautics, 1949), by Stanley H. Scher, Lawrence J. Gale, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Calculated values of transient and steady state performance characteristics of man-carrying, cargo, and extraction parachutes (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1966), by Eugene L. Haak, Richard V. Hovland, Wright-Patterson Air Force Base (Ohio), University of Minnesota, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Analytical and experimental investigation of supersonic parachute phenomena (Wright-Patterson Air Force Base, Ohio : Flight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by L. W. Sims and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Stress analysis of a fully inflated ribless guide surface parachute (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1965., 1965), by H. G. Heinrich, Lelan R. Jamison, Air Force Flight Dynamics Laboratory (U.S.), and University of Minnesota (page images at HathiTrust)
• Aerodynamic characteristics of an ejection seat escape system with a stabilization parachute at Mach numbers from 0.3 through 1.2 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), by David E. A. Reichenau, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Wake properties behind an ejection seat escape system and aerodynamic characteristics with stabilization parachutes at Mach numbers from 0.6 to 1.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), by David E. A. Reichenau, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)

• Stress analysis of a parachute during inflation and at steady state (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), by H. G. Heinrich, Lelan R. Jamison, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)

• A study of canopy shapes and stresses for parachutes in steady descent (Wright-Patterson Air Force Base, Ohio : Wright Development Center, Air Research and Development Command, United States Air Force, 1955., 1955), by A. D. Topping, N. C. Costakos, J. D. Marketos, Wright Air Development Center, and Goodyear Aircraft Corporation (page images at HathiTrust)

• Deployment, dynamic stability, and control characteristics of a 1/12-scale dynamic radio-controlled model of a large booster and parawing (NASA, 1963), by Sanger M. Burk, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• NASA TN D-6300 (National Aeronautics and Space Administration ;, 1971), by Earle K. Huckins, Lamont R. Poole, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Study of parachute opening : Phase I (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1956., 1958), by J. R. Foote, J. B. Giever, United States. Air Force. Air Research and Development Command, University of Oklahoma, and Wright Air Development Center (page images at HathiTrust)
• Study of parachute opening : Part II (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by J. R. Foote, J. B. Giever, United States. Air Force. Air Research and Development Command, University of Oklahoma, and Wright Air Development Center (page images at HathiTrust)
• Infinite mass operating case (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1966., 1966), by H. D. Melzig, P. K. Schmidt, Deutsche Forschungsanstalt für Luft- und Raumfahrt (1961-1969), and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)

• Deployment of a parawing recovery device for a radio-controlled 1/5-scale dynamic model spacecraft (NASA, 1963), by Charles E. Libby, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of parachute opening : Phase I (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1956., 1958), by J. R. Foote, J. B. Giever, United States. Air Force. Air Research and Development Command, University of Oklahoma, and Wright Air Development Center (page images at HathiTrust)
• Study of parachute opening : Part II (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by J. R. Foote, J. B. Giever, United States. Air Force. Air Research and Development Command, University of Oklahoma, and Wright Air Development Center (page images at HathiTrust)

• Law enforcement simulation model (LESIM) : a support tool for planners and decision makers (U.S. Coast Guard, Office of Engineering, Logistics, and Development ;, 1995), by Kevin F. Downer, Christopher M. Rodriguez, Kevin J. Cavanaugh, Logistics United States. Coast Guard. Office of Engineering, and U.S. Coast Guard Research & Development Center (page images at HathiTrust)

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