Aerodynamic Characteristics Of Towed Cones Used As Decelerators At Mach Numbers Rom 1 57 To 4 65

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Index To Nasa Technical Publications

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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960-07

Index To Nasa Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960-07 with categories.

Journal Of The British Interplanetary Society

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Author : British Interplanetary Society
language : en
Publisher:
Release Date : 1934

Journal Of The British Interplanetary Society written by British Interplanetary Society and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1934 with Rockets (Aeronautics) categories.

Cumulative Title Index To United States Public Documents 1789 1976

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Author : Sandra K. Faull
language : en
Publisher: Arlington, Va. : United States Historical Documents Institute
Release Date : 1979

Cumulative Title Index To United States Public Documents 1789 1976 written by Sandra K. Faull and has been published by Arlington, Va. : United States Historical Documents Institute this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Reference categories.

The Aeronautical Journal

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Author :
language : en
Publisher:
Release Date : 1970

The Aeronautical Journal written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Aeronautics categories.

Aerodynamic Characteristics Of Towed Cones Used As Decelerators At Mach Numbers Rom 1 57 To 4 65

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Author : Nickolai Charczenko
language : en
Publisher:
Release Date : 1962

Aerodynamic Characteristics Of Towed Cones Used As Decelerators At Mach Numbers Rom 1 57 To 4 65 written by Nickolai Charczenko and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Aerodynamics categories.

Towed and sting-supported cones were tested in the wake of various payloads at supersonic speeds to determine their drag and stability characteristics. The investigation extended over a Mach number range from 1.57 to 4.65 and included such variables as Reynolds number, cone angle, ratio of cone base diameter to payload base diameter, and trailing distance. Cones towed in the wake of a symmetrical payload at supersonic speeds, in general, had good drag and stability characteristics if towed in the supersonic flow region. A cone with an included angle between 80 and 90 degrees gave 2 maximum drag while still maintaining stability. In order to minimize wake effects, the ratio of cone base diameter to payload base diameter should be at least one and preferably around three. A trailing distance of three times the payload base diameter, in most cases, is of sufficient length to avoid low drag and instability of the decelerator. (Author).

Bulletin Signal Tique

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Author :
language : fr
Publisher:
Release Date : 1963

Bulletin Signal Tique written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Physics categories.

Aerodynamic Characteristics Of Towed Spheres Conical Rings And Cones Used As Decelerators At Mach Numbers From 1 57 To 4 65

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Author : Nickolai Charczenko
language : en
Publisher:
Release Date : 1963

Aerodynamic Characteristics Of Towed Spheres Conical Rings And Cones Used As Decelerators At Mach Numbers From 1 57 To 4 65 written by Nickolai Charczenko and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Cone categories.

An investigation was made to determine the drag and stability characteristics of the various decelerators when towed in the wake of several space-vehicle configurations at Mach numbers from 1.57 to 4.65. The following parameters were varied: Reynolds number, trailling distance, ratio of deceleration base diameter to space-vehicle base diameter, cone angle, and size of disk added to the base of a cone.

Aerodynamic Characteristics Of Towed Cones Used As Decelerators At Mach Numbers From 1 57 To 4 65

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Author : Nickolai Charczenko
language : en
Publisher:
Release Date : 1961

Aerodynamic Characteristics Of Towed Cones Used As Decelerators At Mach Numbers From 1 57 To 4 65 written by Nickolai Charczenko and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.

Towed and sting-supported cones were tested in the wake of various payloads at supersonic speeds to determine their drag and stability characteristics. The investigation extended over a Mach number range from 1.57 to 4.65 and included such variables as Reynolds number, cone angle, ratio of cone base diameter to payload base diameter, and trailing distance. Cones towed in the wake of a symmetrical payload at supersonic speeds, in general, had good drag and stability characteristics if towed in the supersonic flow region. A cone with an included angle between 80 and 90 degrees gave 2 maximum drag while still maintaining stability. In order to minimize wake effects, the ratio of cone base diameter to payload base diameter should be at least one and preferably around three. A trailing distance of three times the payload base diameter, in most cases, is of sufficient length to avoid low drag and instability of the decelerator. (Author).

Aerodynamic Characteristics Of Spherically Blunted Cones At Mach Numbers From 0 5 To 5 0

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Author : Robert V. Owens
language : en
Publisher:
Release Date : 1965

Aerodynamic Characteristics Of Spherically Blunted Cones At Mach Numbers From 0 5 To 5 0 written by Robert V. Owens and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aerodynamics categories.

Results Of A Free Flight Test To Determine The Performance Characteristics Of A Towed Conical Decelerator

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Author : J. W. Usry
language : en
Publisher:
Release Date : 1969

Results Of A Free Flight Test To Determine The Performance Characteristics Of A Towed Conical Decelerator written by J. W. Usry and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Results of a Free-Flight Test to Determine the Performance Characteristics of a Towed, Conical Decelerator categories.

An inflatable fabric decelerator was tested in free flight to determine its drag and stability characteristics. The inflated decelerator approximated an 80 cone with a 48 inch (121.9) base and was towed behind a cone cylinder flare payload at a distance of 13.6 feet (4.15 m) from payload base.