[PDF] Performance Characteristics Of A Preformed Elliptical Parachute At Altitudes Between 200000 And 100000 Feet Obtained By In Flight Photography eBook

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Performance Characteristics of a Preformed Elliptical Parachute at Altitudes Between 200,000 and 100,000 Feet Obtained by In-flight Photography

Charles H. Whitlock
Performance Characteristics of a Preformed Elliptical Parachute at Altitudes Between 200,000 and 100,000 Feet Obtained by In-flight Photography by Charles H. Whitlock PDF

Author : Charles H. Whitlock
Publisher :
Page : 38 pages
File Size : 22,40 MB
Release : 1964
Category : Parachutes
ISBN :

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The performance characteristics of a preformed elliptical parachute at altitudes between 200,000 and 100,000 feet have been obtained by means of in-flight photography. It was demonstrated that this type of parachute will open at altitudes of about 200,000 feet if conditions such as twisting of the suspension lines or draping of the suspension lines over the canopy do not occur. Drag-coefficient values between 0.6 and 0.8 were found to be reasonable for this type of parachute system in the altitude range between 200,000 and 100,000 feet.

Performance Characteristics of a Preformed Elliptical Parachute at Altitudes Between 200,000 and 100,000 Feet Obtained by In-flight Photography

Charles H. Whitlock
Performance Characteristics of a Preformed Elliptical Parachute at Altitudes Between 200,000 and 100,000 Feet Obtained by In-flight Photography by Charles H. Whitlock PDF

Author : Charles H. Whitlock
Publisher :
Page : 25 pages
File Size : 32,13 MB
Release : 1964
Category : Parachutes
ISBN :

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The performance characteristics of a preformed elliptical parachute at altitudes between 200,000 and 100,000 feet have been obtained by means of in-flight photography. It was demonstrated that this type of parachute will open at altitudes of about 200,000 feet if conditions such as twisting of the suspension lines or draping of the suspension lines over the canopy do not occur. Drag-coefficient values between 0.6 and 0.8 were found to be reasonable for this type of parachute system in the altitude range between 200,000 and 100,000 feet.

A Selected Listing of NASA Scientific and Technical Reports for ...

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
A Selected Listing of NASA Scientific and Technical Reports for ... by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division PDF

Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher :
Page : 1156 pages
File Size : 10,16 MB
Release : 1964
Category : Aeronautics
ISBN :

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